Contents


Introduction

The design of the AGC went through several stages, which for the sake of this discussion we'll call "blocks".  However, the different block designs, while similar in many ways, were quite different in others.  Rather than try to cover all of them on this one page, the different blocks are covered in separate pages:

However, this page confines itself just to the Block I design.

It would be very easy, I think, particularly if you only looked at it very superficially, to dismiss the Block I AGC as a computer that was merely a rebranded but otherwise almost-identical version of the Block II.  But in fact, I think it would be fairer to say that in spite of family resemblances, these are quite-different machines for which somebody went to a lot of difficulty to make the development experiences seem very similar.  Having dealt with both of them at some level of detail, I'll say that using what you know about the one with the other is a quick path to frustration.

Here is a nice little 30-minute documentary in which the Block I AGC and DSKY are demonstrated and various interesting details of their internal construction and manufacture are discussed, by people such as Eldon Hall, Albert Hopkins, and Ramón Alonso, whose names you will see mentioned elsewhere on this page and this site:



Available Documentation

Descriptive material about the Block I AGC is not quite as abundant as for the Block II, but it has become distinctly less shabby over time.  Here's what I think of as being the principal sources of information:
  1. R-410:  General Design Characteristics of the Apollo Guidance Computer, by Eldon C. Hall, May 1963.
  2. Lots and lots of the official MIT/IL electrical-schematic and mechanical drawings.  I would be lying if I said our engineering-drawing collection is 100% complete, but we have a stunning level of detail on eight different models of the Block I AGC, assuming I haven't miscounted, and on a similar array of Block I DSKYs.  If you could get the components that the engineering drawings use, you could build a working Block I AGC and DSKY from them.
  3. AC Electronics document ND-1021041 (volume 1 and volume 2).  This is essentially a theory-of-operation document for the Block I AGC and DSKY, and indeed even contains its own set of electrical schematics which often seem to be slightly later revisions than the official MIT/IL drawings mentioned above.
  4. R-393:  Logical Description for the Apollo Guidance Computer (AGC 4), by Albert Hopkins, Ramon Alonso, and Hugh Blair-Smith, July 1966.
  5. FR-2-102A, "Apollo Guidance Computer Information Series, Issue 2: Machine Instructions", 03/10/1963, by Raytheon.
  6. FR-2-106A, "Apollo Guidance Computer Information Series, Issue 6: Interpreter and Interpretive Instructions", 09/25/1963, by Raytheon.
  7. FR-2-106B, "Apollo Guidance Computer Information Series, Issue 6B: Interpreter and Interpretive Instructions", 05/29/1964, by Raytheon.
  8. ... and other of the Apollo Guidance Computer Information Series.
  9. R-467:  The Compleat Sunrise being a description of Program Sunrise (Sunrise 33 - NASA DWG# 1021102), by R. Battin, R. Crisp, A. Green, T. J. Lawton, C. A. Muntz, J. Rocchio, and E. Smally, September 1964.
  10. E-1574: Keyboard and Display System Program for AGC (Program SUNRISE), by Alan I. Green and Joseph J. Rocchio, August 1964.
  11. John Pultorak's Block I simulator source code.
  12. Solarium 055 (Apollo 6 unmanned mission) assembly listing, December 4, 1966.
  13. Personal communications by Hugh Blair-Smith.
  14. Hugh Blair-Smith's book, Left Brains for the Right Stuff, or as he refers to it, LB4TRS.

Of these, MIT/IL document R-393 is the principle documentation of the Block I computer system — or at least it was prior to obtaining engineering drawings and ND-1021041 as mentioned above — but it is important to recognize that its descriptions are not entirely accurate.  By this I mean not merely that it contains mistakes — as, indeed, any documentation of a sufficiently-complex system will — but that the design of the system was extended after document R-393 was written, so that some of the later-superceded information in it is blatantly wrong to the point of making anything based on it non-functional. The most-glaring discrepancy is the memory map, which R-393 describes as being 1024 words of read/write memory and 12 1024-word banks of read-only memory, whereas there were in fact 24 banks of read-only memory by the time of the Solarium (Apollo 6 unmanned mission) software mentioned above.   In other words, Solarium wouldn't have fit into the amount of memory R-393 describes. 

Finally, it's worth noting that people often seem to believe that the electrical schematics of the Block I AGC are contained in the original PDFs which John Pultorak published of his Block I AGC simulation.  While those are fine schematics, and worked well for John's purposes, they are not transcriptions of the original Block I schematics, but are rather schematics John designed from scratch, based on the textual descriptions he found in R-393.  In the first of his PDFs, there is a detailed diary of what he did, and everything in it refers back to R-393, but not to the original schematic diagrams of the Block I, which were not available to him.  Thus, while John's work on reverse engineering the Block I AGC essentially from R-393 alone is a stunning tour de force — after all, his gadget ended up working! — his schematics may or may not be valuable resources for you, depending on your purposes.


Block I Computer System

Computer

The Block I AGC was provided in two different configurations, one for the Command Module (then referenced as the C/M), and one for the Lunar Module (at that time still called the LEM, or Lunar Excursion Module).  Even though personally still bummed out (fifty years later) over the change from LEM to LM, for consistency I'll refer to the spacecraft here as the CM and LM and forego the temptation to instead talk about the LEM.

The physical configurations of these were different in terms of form factor, weight, and memory capacity — and of course, software — and here are the highlights:

Of course, that's merely the summary.  If you really wanted full details of what the Block I AGC was like, then you'd have to narrow your focus to just the specific mission you were interested in and consult the engineering drawings themselves.  In fact, here are some links to those engineering drawings for the Block I (unmanned) missions flown:

That's not to say that those were the only versions of the Block I AGC, and there were plenty more that never went on a flown mission!  On the other hand, also not intended to imply that all of these models were very different.  They were, after all, completely compatible in terms of the software they could run.

No Block I LM missions ever flown, and I'm not aware of any Block I LM software, so I can't comment on whether the LM Block I AGC requirements listed above are accurate.





The first two pictures above depict the CM Block I AGC (which I've poorly reproduced from Eldon C. Hall's book, Journey to the Moon: The History of the Apollo Guidance Computer, which you should buy), while the final one depicts the LM version (sorry there's no better picture), taken from document R-410, by ... wait for it ... Eldon C. Hall.

Incidentally, a fellow named Francois Rautenbach has recently (at least, it was recent at the time I'm writing this) been engaged in extracting the contents of the core memory from the Block I AGC used for unmanned AS-202 mission, sometimes known as "Apollo 3".  As a part of that effort, or vice-versa (I'm not sure which), he has also been making a series of YouTube videos in which there's a lot of info and there are nice visuals about the Block I AGC (and the Block II as well), beyond what the poor photographic reproductions above can reveal.  Well worth viewing!

DSKY

As in Block II, the DSKY was the display/keyboard unit with which an astronaut could have entered data into the computer and gotten feedback from it.  Block I DSKYs differed from Block II DSKYs, and even from each other.  Recall that the Command Module had two DSKYs (even though it had only one AGC), one on the main control panel and one on the navigation side-panel.  The second DSKY was used for entering star or other landmark location sightings.  In a Block II CM, the main and nav DSKYs are identical.  In a Block I CM, on the other hand, the main and nav DSKYs were different.

Block 1 DSKY, nav bay   

The left-hand picture above is a nav-bay DSKY.  On the right is a photo of a main control-panel DSKY.

And just how big were they?  Well, in the picture to the right, you see Eldon Hall standing next to one of the control-panel DSKYs, so the answer is, they were very, very big!  A nav-bay DSKY has the same push-button sizes as the control-panel DSKY and would have reached nearly to Eldon's shoulder, if sitting on the same table.

We have many of the engineering drawings as well, so you could certainly consult those if you were a connoisseur or glutton for technical detail:
Below are some drawings from a set of Apollo Guidance and Navigation System training slides, which are perhaps of greater value if your interest is casual.  If you click the drawing of the nav-panel DSKY (on the left), you can get a larger view in which the text is actually legible.



From our (or perhaps my) standpoint, the most-important characteristic of the DSKY is that it is a very dumb device, in the sense that it is close to being just a set of lights and push-buttons connected directly to electrical outputs and input of the AGC.  This is not entirely true, since there would simply be too many such signals if each were provided with it's own dedicated wire, so some of the signals are multiplexed together, latched into internal relays provided by the DSKY.

Outputs from the DSKY to the AGC are the states of the pushbuttons on the keypad.  These simply directly control 6 bits on the CPU's IN0 register.  Refer to bits B1-B6 of the IN0 register in the "I/O Channels" section below.

Outputs from the AGC's OUT0 and OUT1 registers control the DSKY's indicator lamps, octal/decimal displays, and the special "flashing" feature which can cause the illumination of the VERB and NOUN labels to flash on and off.  The octal/decimal (7-segment displays plus signs) are controlled by the multiplexing feature mentioned earlier.  Each 15-bit word placed into the OUT0 register consists of 4 bits (a "relay word") that specify a particular set of 11 relays in the DSKY, while the other 11 bits specify the data that's supposed to be latched into those relays.  In theory, up to 16*11=176 separate relays could be present, and thus 176 signals could be multiplexed by this scheme; in reality, only 11 of the possible 16-bit relay words are used, and not all of their bits are used, so only 113 of the possible 176 bits are actually used.

Uncertainties:

Uplink

The digital uplink was simply a way to have a remote keypad on the ground, which could transmit keystrokes via radio to the AGC aboard the spacecraft as if it were a DSKY.  In other words, the only data the uplink could transmit corresponded to DSKY keypad codes.  The keycodes were identical to the 5-bit DSKY keycodes as described in the preceding section, but if (say) a 5-bit keycode of bits B5 B4 B3 B2 B1 were to be transmitted, they were supposed to be packaged into the following 16-bit format for the uplink:

1 B5 B4 B3 B2 B1 B5 B4 B3 B2 B1 B5 B4 B3 B2 B1

where the overbar implies the logical-complement of the bits: 0 is replaced by 1 and vice-versa.  The uplink was, of course, serial: the leading 1 was transmitted first, and the least-significant B1 last.  As each bit was received, it was shifted into the least-significant bit of the CPU's UPLINK register at address 041, which was initially all zero, and the other bits in the register were shifted upward by one position.  When bit 16 of the register eventually became 1, an UPRUPT interrupt was triggered, and the AGC's UPRUPT interrupt-service routine could read the register, zero it, and process the data it had received.  Of course, the way the data was packaged within the transmitted word, it was triply redundant and could thus be checked for corruption and discarded if it was found to be corrupted. 

After the uplink was detected, the UPTL activity lamp on the DSKY illuminated to inform the astronauts that an uplink was in progress, and it remained illuminated in most cases until the uplink sent a KEY RLSE keycode to "release" the uplinked keypad.

There was a toggle switch on the DSKY that could be used either to allow uplinked data, or else to block it and allow the spacecraft and/or astronauts to retain complete control of the keypad input.  If the uplink was allowed, then the uplinked keycodes were treated indistinguishably (at least superficially) to keypad input, and the results of the input could be seen on the DSKY.  For example, an uplinked V36E would be seen visibly on the DSKY as the VERB area first blanking out, then a 3 appearing, a 6 appearing, and finally, a fresh start being performed, since "fresh start" is the purpose of a V36E.  Naturally, the DSKY could not be seen physically on the ground, and the digital-uplink itself did not provide any feedback to the ground as to the effect the remote keystrokes were having aboard the spacecraft.  That feedback, among other things, was the responsibility of the digital downlink as covered in the next section.

Downlink

TBD

Other Peripherals

What the MIT Instrumentation Laboratory designed and provided for the Block I Command Module included not merely the AGC and its DSKYs, but rather than entire Guidance & Navigation (G&N) systems for the Command Module.  The G&N system consisted of quite a few additional components, of which some of the more important were:

In some sense, the IMU is the most important of all, more so than the AGC and DSKY, since (I believe) the IMU was what Doc Draper originally developed and attempted to hawk to the military, and was the Instrumentation Lab's entrée into Apollo in the first place.  The IMU existed long before the AGC was even a gleam any any designer's eye.  The AGC and DSKY, from that point of view, were just a way of interacting with the IMU, and without the IMU there really wasn't much of an excuse for MIT/IL to be involved in Apollo at all.  But since our focus here is really just the AGC and DSKY, I won't really be covering these other very-important "peripheral" components at all.

Nevertheless, if you want to know about them we do still have quite a collection of documents and engineering drawings covering the entire G&N system.  Here's a portal into electrical and mechanical engineering drawings for the flown versions of the Block I G&N system:


Computer Hardware Architecture

Memory Map

The Block I AGC memory map is far simpler than that of the Block II AGC.

Memory is divided into 02000 (octal) mostly 15-bit words of "erasable" memory — i.e., memory which can both be read from and written to — and 24 banks, each with 02000 words, of read-only or "fixed" memory.

Conventionally, AGC programming uses octal notation, as opposed to decimal or hexadecimal notation, for most purposes, and I'll do that below, but I'll try to remember to prefix an extra 0 to the front of an octal number to make it easy to recognize as being octal.  For example, if you see 15, you'll know that it's 15 decimal because there's no leading zero, whereas of you see 015, you'll know that it's octal (=13 decimal).  That's only a convention on this page; in program listings or conversations with AGC developers (assuming you find yourself in a position to engage in such an activity), expect to see everything in octal with no leading zeroes, and don't expect anybody to mention hexadecimal, and only occasionally to encounter decimal numbers.

Memory is laid out as follows:
Thus, fixed memory locations can always be referred to as
BB,AAAA
where BB is an octal bank number from 01 to 034, and AAAA is an octal offset into that bank from 06000 to 07777.  Only banks 01 and 02 have the special short addresses 02000 through 05777, and they are invariably referred to in that way rather than in the BB,AAAA form.

Various erasable-memory locations in the address range 0-057 have special purposes, such as being dedicated CPU registers, input/output ports, or counters (such as system timers).

15 Bits, 16 Bits, Parity, 1's-Complement, and Overflow

The information in this section should not differ from equivalent information for Block II, so if you are confident you understand that, then there's no reason to read it.  However, it is not merely cut-and-pasted from corresponding Block II descriptive material, and so may (or may not) be useful in itself.

Almost all AGC memory words consist of 16 bits, of which 15 bits is "data", and a 16th bit is a parity bit that the AGC hardware can access for the purpose of testing for corruption.  If you were to build an AGC or to create a hardware simulation of an AGC, that parity bit would be an important thing to understand and account for, since parity violations are detectable by hardware, cause alarm indicators to trigger, and so on.

On the other hand, my own preoccupation in this site, in so far as Block I is concerned, is making Solarium and other Block I programs available within a software simulation of the AGC.  Parity is completely irrelevant to that usage, because such an environment is not an embedded one, and parity is just a confusing distraction ... so I don't care about parity, my software simulation doesn't care about parity, and I won't mention parity again.  As one of the original AGC developers commented to me, "parity schmarity", and I think that about sums it up.  Consequently when I talk about AGC memory, it will almost always be in terms of 15-bit words.

But there are some exceptions.  Certain reserved memory locations, which aren't always (strictly speaking) contained in erasable memory even though addressed as such, consist of 16 bits, but  the 16th bit is not parity; rather, it is an indication of "overflow".  The principal example of such a privileged location is the "accumulator register", A, discussed in the next section.  That's because all results of most kinds of arithmetical operations are deposited directly into the accumulator, and if an operation such addition has overflowed, that will first be manifested in the accumulator.  Various subsequent operations on that data will behave differently depending on whether or not (or how) overflow is manifested within the accumulator.  There are also hidden registers, not addressable by software, and overflow within those registers may have significant implications just like overflow in the accumulator does.

I have been chided for liking to think of "overflow" is if it were a condition that has occurred, such as "the accumulator has wrapped around from positive to negative" and thus overflowed, or "the accumulator has wrapped around from negative to positive".  That's a poor way to think about overflow in this architecture, for a couple of reasons:

  1. Arithmetical overflow does not "wrap around", in the sense of changing sign, because the AGC employs 1's-complement arithmetic rather than 2's-complement arithmetic.  Wrap-around with sign-change is a characteristic of 2's-complement arithmetic.  However, with 1's complement, overflow does not work that way.  If, say, you add 1 to the largest possible positive number, it will indeed wrap around, but it will wrap around to +0 and not to a negative value.
  2. Overflow is not an instantaneous condition that disappears, but rather is encoded within the 16-bit value, and continues to be manifested there until some operation occurs which converts the value back to a 15-bit one incapable of retaining the overflow information.

Before getting to the exact encoding of overflow information, though, let's briefly talk about the 1's-complement representation of numbers.  Consider a 15-bit number with bits B15 B14 ... B1.  This representation can store 214-1=16383 distinct positive numbers (1 through 16383), and 214-1=16383 distinct negative numbers (-1 through -16383).  Zero actually has two distinct representations, +0 and -0, which act the same for some purposes and differently for others.  In other words, +0 and -0 are not completely interchangeable with each other.  The positive numbers are encoded the same way they would be in 2's-complement:

0 (decimal) = 000 000 000 000 000 (binary)
1 (decimal) = 000 000 000 000 001 (binary)
2 (decimal) = 000 000 000 000 010 (binary)
3 (decimal) = 000 000 000 000 011 (binary)
4 (decimal) = 000 000 000 000 100 (binary)
...
16383 (decimal) = 111 111 111 111 111 (binary)

Negative numbers, in the other hand are not encoded the same way, but are simply the logical complements of the corresponding positive numbers.  For example,
12345 (decimal) = 011 000 000 111 001 (binary)

so

-12345 = 011 000 000 111 001 = 100 111 111 000 110

Now, in 1's-complement there is no "sign bit" as such.  In other words you can't turn (say) 3 into -3 or vice-versa by just flipping one bit.  Nevertheless, in the examples above, the most-significant bit, bit 15, does indicate the sign, and therefore you can tell whether a number is positive or negative by testing bit 15.  For that reason, bit 15 is sometimes called the "sign bit" and is sometimes designated by the special symbol

SG = bit 15 = "sign bit"

For those special 16-bit memory locations, like the accumulator, a regular, non-overflowed number will have its 16th bit identical to its 15th bit.  It also has a special designation:

UC = bit 16 = "uncorrected sign bit".

In other words, for numbers without overflow, SG = UC (=0 if positive or =1 if negative).  For numbers with overflow, though, this is not the case.  There are two possibilities for numbers with overflow:

The tricky aspect here is that when overflow exists, it is UC that is regarded as the "real" sign of the number, and not UC.  When the 16-bit form of a number (say, in the accumulator) needs to be converted to a normal 15-bit number (say, to be stored at a location in erasable memory), what happens is that the UC bit steps in and kicks the SG bit out of the way:

UC SG B14 ... B1 (16 bits)  →  UC B14 ... B1 (15 bits)

Let's consider an example of this in action.  Imagine we want to increment the largest possible positive number, 037777, by 1.  Start by just using the same old binary arithmetic you're familiar with, without worrying about "1's-complement" vs "2's-complement" or overflow:

0 011 111 111 111 111 + 0 000 000 000 000 001  →  0 100 000 000 000 000

Having done that, though, we now have overflow, and specifically "positive overflow", since UC = 0 and SG = 1 do not agree with each other.  And if we were to save this as a 15-bit number, UC = 0 would shift down to overwrite the SG = 1, and we'd simply have 000 000 000 000 000, or just 0.

Registers

Incidentally, note that while I (and everybody else) refer to the registers I'm going to discuss by their names rather than their addresses, the assembler is in fact not aware of those names; they are not reserved words or predefined.    Therefore, a program like Solarium will contain pseudo-ops that define these names as having the numerical values of the registers' addresses.

There are 4 16-bit registers addressable directly by software and partaking of the 16-bit glory of overflow, UC, and SG discussed in the preceding section.

There's also a variety of 15-bit registers:

You might suppose that since the various RUPT registers mentioned above are 15-bit, but the values which are supposed to be stored in them are 16-bit, that this could cause a problem.  In fact, though interrupts are inhibited when A or B contain overflow, so they cannot cause a problem.  As far as Q, Z, and LP are concerned, while they may theoretically have 16 bits, there is seldom any useful way to use the 16th bit, and for those cases one could use the INHINT instruction (discussed later) to inhibit interrupts during a short stretch of code where it might be a problem.

In the list above, I've left out a number of registers related to i/o or used as timer/counters, and those are covered in the succeeding sections.

I/O Channels

Unlike the Block II system, there is no separate i/o-channel address-space, and the i/o channels are simply memory mapped.  Even so, we'll discuss them separately from the other registers. There are  4 15-bit input channels and 5 15-bit output channels. These are not all fully (or correctly) documented in the R-393 or "Compleat Sunrise" documents, and haven't yet been entirely vetted by me or my colleagues, so you have to take some of them with a grain of salt; that's particularly true when you see a terse description like "1600 pps" as opposed to a more drawn-out description with my signature verbosity.

The least-significant bit of these registers is referred to below as B1, and the most-significant as B15: To understand the various fields (WWWW, S, AAAAA, BBBBB) used in the OUT0 word, you have to be able to relate them to the various sets of 7-segment displays and +/- sign displays on the DSKY.  Examine the following diagram, which is a stylized representation of the area on the DSKY containing the numerical displays:
                               PROGRAM
                             [MD1] [MD2]

    VERB                         NOUN
[VD1] [VD2]                  [ND1] [ND2]

               REGISTER 1
[R1S] [R1D1] [R1D2] [R1D3] [R1D4] [R1D5]

               REGISTER 2
[R2S] [R2D1] [R2D2] [R2D3] [R2D4] [R2D5]

               REGISTER 3
[R3S] [R3D1] [R3D2] [R3D3] [R3D4] [R3D5]
Thus, each one of the designations in [brackets] represents a displayed digit or else a +/- sign.  For example, [VD1] is the left digit of the "verb".  The value of each of signs is determined by a particular combination of WWWW and S fields, while each of the digits is determined by a particular combination of WWWW and AAAAA or BBBBB fields.  The specific mapping used is:

WWWW
S
AAAAA
BBBBB
017
(cannot occur)
016
(see below)
015
(see below)
014
(see below)
013
n/a
MD1
MD2
012
FLASH
VD1
VD2
011
n/a
ND1
ND2
010
UPACT
n/a
R1D1
007
R1S +
R1D2
R1D3
006
R1S -
R1D4
R1D5
005
R2S +
R2D1
R2D2
004
R2S -
R2D3
R2D4
003
n/a
R2D5
R3D1
002
R3S +
R3D2
R3D3
001
R3S -
R3D4
R3D5
000
(normal, inactive state)


As you can see, a couple of the S fields don't actually correspond to +/- signs at all.  FLASH refers to the ability of the DSKY to flash the words "VERB" (appearing above VD1 and VD2) and "NOUN" (appearing above ND1 and ND2) about once per second; this feature is active after FLASH is set to 1, and deactivated (with the words remaining lit) after FLASH is set to 0.  The UPACT bit refers to the UPTL activity lamp on the DSKY, and turns that lamp on or off.

However, the principal purpose of OUT0 is to control the digits and +/- signs displayed on the DSKY.  As an example, the R1S sign is displayed as "+" when R1S+ is 1 and R1S- is 0, while the R1S sign is displayed as "-" when R1S+ is 0 and R1S- is 1.  It is blank when both R1S- and R1S+ are 0.  (I'm not sure what it's supposed to display if both are 1.)

The AAAAA and BBBBB fields control what digits are displayed in RnDm, but not in the straightforward fashion of 0=0, 1=1, etc.  Rather,

AAAAA or BBBBB
Displays
000
blank
025
0
003
1
031
2
033
3
027
4
036
5
034
6
023
7
035
8
037
9


So finally, as an example, suppose the value 027576 (WWWW=05, S=1, AAAAA=033, BBBBB=036) is written to OUT0.  Then in REGISTER 2, the leftmost three positions would display "+35".  Since this is latched in the DSKY, those positions continue to display that way until a new word with WWWW=05 is written to OUT0 and are unaffected to writes to OUT0 with different values of WWWW.

Regarding the various combinations of WWWW not covered above:

Counters and Timers

Counter/timer registers are registers in erasable memory which are automatically incremented or decremented by specific actions of the hardware, independent of the operation of the software.  Thus, the software may (in some cases) usefully load an initial value into them, but for the most part just polls the contents of these registers when it needs to do so.  In some cases too, an overflow of one of these registers may trigger an interrupt.

Interrupt Processing

At fixed-memory address 02000, you find a vector-interrupt table, containing 7 interrupt vectors, each 4 words long, which are triggered automatically in the case of an interrupt ... which are referred to as "RUPTS". Actually, the 7th is not an interrupt vector at all, but rather the power-up entry point, but it seems reasonable to lump it in with the other 6.

The different interrupt types are:
An interrupt performs several functions automatically in hardware before the interrupt-servicing by the software begins. The existing Q and Z register values are transferred to the CPU registers QRUPT and ZRUPT, and then an implicit TC instruction transfers control to the interrupt vector code, thus overwriting Q and Z with new values. The interrupt-service routine must eventually be terminated with the RESUME instruction, which undoes those steps ... i.e., it restores Q and Z to their original forms and puts the program counter back to what it had been, the position of the next instruction that was due to be reached when the interrupt occurred.

But note that the instruction stored at that return location is not necessarily the instruction executed at that point! That's because instructions are sometimes preceded in memory by an INDEX instruction (described later) which has the effect of altering the instruction in-place, even though usually stored in fixed memory, by adding something to it in advance. Thus if an interrupt occurs between an INDEX and the instruction being indexed that follows it, it is actually the indexed instruction that will be performed when after the RESUME occurs. The indexed instruction is stored in a special CPU register, BRUPT, while the interrupt is being serviced. This register is so-called because in normal operation the CPU stores the value of the instruction it is executing in a special hidden, non-addressable register called B.

Other than Q, Z, and B, the remainder of the state is not automatically stored during the interrupt, and so the interrupt-service routine has to explicitly store any other data which must be retained, such as the A register.

Only one interrupt can be serviced at a time, and interrupts occurring simultaneously are prioritized in the same order as shown above.
Interrupts can be inhibited in a variety of ways, in which case the interrupts don't occur until the inhibiting factor is removed. These inhibiting factors are:


Software

The Interpreter vs. the CPU's Basic Instruction Set

As mentioned above, the Block I AGC design did not end up being used in any moon missions, nor even in any manned missions, but if it had been used, the required software could not have been fit into the memory provided by the Block I unit if simply written in the AGC CPU's native assembly language.  (Nor even in the Block II computer, as described here.)  Consequently, as with the Block II design, both the native low-level assembly language (referred to as "basic") and a higher-level language (referred to as "interpreter") were supported by the system, and a Block I program is an intermixture of both of these two programming languages.

Because each of the interpreter's instructions represented many AGC assembly-language instructions, a larger amount of functionality could be fitted into the same amount of core memory, even accounting for the fact that software was needed to implement the interpreter. The drawback was that implementing any particular functionality in interpretive language required far more execution time than implementing the same functionality directly in AGC assembly language. But as long as the program ran "fast enough", that didn't matter very much.  Between an assembly-language block of code and an interpretive block of code, there will be a call (in assembly language) to the interpreter subroutine.  In other words, the interpreter subroutine expects to find the code it is going to interpret following the assembly language instruction which called it.  Similarly, a block of interpretive code ends with a specific interpreter instruction meaning "stop interpreting and jump to the next location in memory".

Because of this intermixing, both assembly language and interpretive language have to be understood for effective programming of the device.

Source-Code Formatting Information

The Virtual AGC project's AGC assembler program is known as yaYUL.

The format of source code accepted by yaYUL differs slightly from that accepted by the original YUL assembler, and thus reflected in the assembly listings created by YUL. This is partly because I didn't originally have any documentation for YUL, thus determining the exact format required by it wasn't really possible; but also, formatting restrictions based on strict column alignment—which make a lot of sense with punch-cards—make little sense now that punch-cards have gone to their final resting place.  Thus, yaYUL accepts a format for the Block I source code which is almost independent of column structure but nevertheless ends up providing you with basically the same visual experience.

Here are the principles used in formatting Block I yaYUL source files, along with my stylistic preferences:
These principles are perhaps best understood by viewing actual source-code listings from Solarium 055.

Data Representation

Numerical formats are identical to those for the Block II AGC, and I advise you to read the description of them that appears in the Block II discussion.

Basic Instruction Representation

The instruction set is far smaller, and therefore far simpler, than in Block II.  Every assembly-language instruction occupies precisely one word of memory (including operand), and consists of 15 bits as follows:

CCC AAA AAA AAA AAA

The 3-bit field CCC represents the instruction type (the "code"), while the 12-bits AAAAAAAAAAAA represent a memory address.  With this simple scheme, there are seemingly at most 8 instruction types, each of which can operate on any memory location within a 4096-word area of memory.

Although, actually, more instruction types were packed into this format than just the 8 that would seemingly be allowed by the 3 available bits CCC.  The extra instructions were available in a couple of obvious ways, and in one very subtle, unobvious way.

One of the "obvious" ways, of course, is that just as with the Block II basic instructions, certain special opcode+operand combinations are simply set aside and used differently that one would anticipate.  These will be covered in the next section, but for example:  If the INDEX instruction has the specific operand 017, then it is no longer an INDEX operation, but rather as an INHINT operation.  The other "obvious" way is that certain operations on erasable memory don't make sense for fixed memory, or vice-versa, so their action is different depending on which memory area it applies to.  For example, the XCH opcode — which means to exchange the contents of the accumulator register with an erasable memory location — is instead interpreted as a CAF instruction — which means to load the accumulator from fixed memory — when the operand is a fixed-memory location.

The "subtle" way is to use the INDEX instruction in an unusual way.  The purpose of an INDEX, which is covered in the next section, is to arithmetically add a value to the next instruction following it, and this is typically used for accessing an array by adding (or subtracting) a value from the operand of the instruction.  However, depending on the value being added or subtracted, it could also be used to change the opcode as well.  The most-subtle use, though, is that it's theoretically possible to use INDEX to add a value to the next instruction's opcode which will not only change the opcode, but could actually have a 16th bit which is non-zero, and that 16th bit allows you to add a 4th bit CCCC to the number of instruction types you can have!  In fact, there, are three different types of such "extended" instructions, MP, DV, and SU, all of which will be covered in the next section.  What's fascinating about these instructions is that they are encoded in precisely the same way as the CS, TS, and AD instructions, respectively, and there's literally no way to tell which is which unless you know the instruction that preceded them.  Even more fascinating, while the usual case would be that the preceding instruction was an INDEX operation that just added a constant value, in which case it's easy to that the instruction following it is "extended", sometimes the INDEX'ing was done by adding a variable to the instruction, in order to multiply, divide, or subtract an array element.  In that case, even looking at the preceding INDEX instruction isn't enough to tell you that the next instruction is "extended": to determine that you have to know the value of the variable, which is hard to know without actually executing the code.  Of course, executing the code is no problem for the CPU itself, since that's what the CPU does, but it's a problem for someone (say) disassembling the code, and fortunately it was done extremely rarely.

Basic Instruction Set 

In reading about the effects of the various "basic" instructions below, there are several notational conveniences that you should be aware of:

As for why it may be necessary to distinguish "before" from "after", one reason is the so-called "editing registers" discussed earlier, namely LP, CYR, SR, CYL, and SL.  Recall that when you write to such a register, what's saved in the register isn't the value you're theoretically writing to it, but rather an "edited" form of that value.  For example, with CYL this editing process is to rotate all the bits to the left.  Some instructions have as a side effect re-writing the operand, denoted (if the operand is K) by

C(K) = b(K)

Thus even though a given instruction is seemingly using its operand as input rather than for output, if the operand is an editing register, it may be automatically rewritten, and that means it will be re-edited every time the instruction is used.

A couple of points about the Block I basic instruction set that may not be obvious at first glance are:

AD

Description:
"Add"
Syntax:
AD K
Operand(s):
K is any address in memory.
Timing:
2 MCT or 3 MCT
Octal:
060000 + K
Notes:
This instruction adds the contents of a memory location to the accumulator:
C(A) = C(A) + C(K)
It does, however, have the side effect
C(K) = b(K)
which means that if K is an editing register, then it will be edited.

It should be noted that for any number x,
x + -x = -0
Moreover, if the accumulator contains overflow after the addition, the OVCTR register is modified as follows, thus taking one extra MCT to do so:
  • If the overflow is positive, then OVCTR is incremented by one.
  • If the overflow is negative, then OVCTR is decremented by one.

CAF

Description:
"Clear accumulator and add from fixed memory"
Syntax:
CAF K
Operand(s):
K is any address in fixed memory (06000-07777).
Timing:
2 MCT
Octal:
030000 + K
Notes:
This instruction loads C(A) with C(K):
C(A) = C(K)
The value is sign-extended before being loaded into the accumulator.

The opcode is numerically identical to the XCH instructions, with the difference being that K is in fixed rather than erasable memory.

CCS

Description:
"Count, Compare, and Skip"
Syntax:
CCS K
Operand(s):
K is any address in fixed memory.  In other words, it cannot be in erasable memory.  If less than 06000 it is in fixed-fixed memory, while if in the range 06000 to 07777 is in banked fixed memory and the Bank register is used to determine the applicable memory bank.  Sometimes the TC occurs then Bank holds 00000, which is actually interpreted as bank 03.
Timing:
2 MCT
Octal:
010000 + K
Notes:
This is used for conditional jumps and for loop control, and has several effects.  K must be in erasable memory, and is thus the address of a variable.  The operand is sign-corrected or sign-extended before use, depending on whether it is from a 16-bit register or 15-bit memory.

The accumulator (A) is loaded with the "diminished absolute value" of the operand,
C(A) = DABS( b(K) )
where DABS(x) is defined as
DABS(x) =
{ |x| - 1, if |x| > 1

+0, if |x| ≤ 1
Also, K is rewritten,
C(K) = b(K)
so K is edited if it is an editing register.

Lastly, a comparison is performed, and a jump is made on the basis of that comparison:
  • Jump to L+1 (i.e., proceed along the normal flow of execution) if b(K) > 0.
  • Jump to L+2 if b(K) = +0.
  • Jump to L+3 if b(K) < 0.
  • Jump to L+4 if b(K) = -0.

If K has a 16th bit (for example, if it is the accumulator), it is the 16th bit (UC) which determines the sign, and not the 15th bit (SG).

Note:  the latter description is at odds with the description on p. 3-4 of R-393, which says that C(K) rather than b(K) is what's tested for the comparison.  But John Pultorak's simulator (and mine) behave the way I've described here, and I trust John's reading of the control-pulse sequences more than I trust R-393.  Of course, John got the pulse sequences from R-393, so it's a vicious cycle!  The issue may need to be revisited later.


COM

Description:
"Complement"
Syntax:
COM
Operand(s):
None
Timing:
2 MCT
Octal:
040000
Notes:
This instruction is actually just a mnemonic for "CS A" and hence just negates (take a bitwise inverse) of the accumulator:
C(A) = -C(A)

CS

Description:
"Clear and Subtract"
Syntax:
CS K
Operand(s):
K is any address in memory.
Timing:
2 MCT
Octal:
040000 + K
Notes:
This instruction loads the accumulator with the negative of the contents of a memory location:
C(A) = -C(K)
which is just the bitwise inverse.  It does, however, have the side effect
C(K) = b(K)
which means that if K is an editing register, then it will be edited.

DOUBLE

Description:
"Double"
Syntax:
DOUBLE
Operand(s):
None.
Timing:
2 MCT or 3 MCT
Octal:
060000
Notes:
This instruction is a mnemonic for "AD A", and hence doubles the accumulator:
C(A) = b(A) + b(A)
If the accumulator contains overflow after the addition, the effect on the OVCTR register is as described for AD.

DV

Description:
"Divide"
Syntax:
DV K
Operand(s):
K is any address in memory.
Timing:
18 MCT
Octal:
050000 + K
Notes:
This is an "extended" instruction, meaning that it is coded as
EXTEND
DV K
or by some operation such as
INDEX K0
DV K
that produces a 16-bit DV instruction value ... i.e., whose bit 16 is non-zero.  Thus even though the octal value of the instruction is shown above as 050000+K, and that's what appears in the rope and how the assembler sees it, in fact by the time it is executed it is really 0120000+K, which is how the CPU sees it.

Logically, though not at the control-pulse level, what you can think of this instruction as doing is:
  1. Multiplying the accumulator by 214.
  2. Dividing that number by the value stored in the operand.
  3. Storing the quotient in the accumulator.
  4. Storing the negative of the absolute value of the remainder in Q.
  5. Setting LP to some positive value if the quotient is positive, or to some negative value if the quotient is negative.
In point of fact, it's not just "some" positive or negative value that's stored in LP, but rather some specific value determined by the control-pulse sequences defining the DV instruction, but R-393 does not define them, and it's impossible to know what they might be without following through the control-pulse sequences in detail. I choose not to do that at this time Unless some AGC developer chose to use his undocumented knowledge of these specific values, which is certainly possible, there should be no need to know the specific values.

This instruction envisages that |b(A)| < |C(K)| but does make some statements about what should happen in other cases
  • If |b(A)| = |C(K)|, then |C(A)| = 037777 and C(Q) = -|C(K)|.
  • If |b(A)| > |C(K)|, then |C(A)| = 037777 and C(Q) "is meaningless".
The latter condition would always be satisfied if the accumulator initially contains overflow, so that condition should be avoided.

C(K) is unchanged, unless K is itself A, Q or LP.

EXTEND

Description:
"Extend"
Syntax:
EXTEND
Operand(s):
None.
Timing:
2 MCT
Octal:
025777
Notes:
This is a mnemonic for special form of the INDEX instruction which is used for producing the necessary overflow in the MP, DV, or SU instruction following it, in a way that enables those instruction types, which would otherwise be interpreted as TS, AD, and MASK instructions.  In other words, the most-straightforward way to use these extended instructions is as
EXTEND
MP K1
...
EXTEND
DV K2
...
EXTEND
SU K3
However, using EXTEND require a little preparation, because the assembler actually treats it as a mnemonic for "INDEX 05777" which will have embarassing results at runtime if the appropriate value isn't actually at address 05777 at runtime.  Solarium uses the following code, which assembles the same as "OCT 47777", so that's what I'd suggest doing:

               SETLOC   5777  # STANDARD LOCATION FOR EXTENDING BITS
OPOVF          XCADR    0
How does this actually work?  Well, suppose you needed to "extend" the instruction SU 1234:

                EXTEND
                SU 1234
These two instructions are the same as INDEX 5777 and OCT 61234, respectively, so when the CPU gets to the SU, the instruction that the CPU will be trying to execute is (because of sign-extension) 0147777+0161234, which equals 0131234 (in 16-bit 1's complement addition, if there's a 1 in bit 17, which there was in this case, it's removed and 1 is added to the number).  The top 4 bits of this 16-bit sum are CCCC=1011, which tells the CPU that it's an SU instruction, but the operand is still 01234.  All of which is, of course, rather convoluted, but it doesn't matter since all you have to remember is that if you stick the EXTEND in front then it magically works.

INDEX

Description:
"Index"
Syntax:
INDEX K
Operand(s):
K is any address in memory other than 016, 017, or 025.  If less than 06000 it is in erasable or fixed-fixed memory, while if in the range 06000 to 07777 is in banked fixed memory and the Bank register is used to determine the applicable memory bank.  Sometimes the TC occurs then Bank holds 00000, which is actually interpreted as bank 03.
Timing:
2 MCT
Octal:
020000 + K
Notes:
This instruction does not affect execution flow — i.e., the next program-counter location after INDEX is at L+1 — but next instruction value used is not C(L+1) but rather C(L+1)+C(K).  In other words, the value stored at K is added to the next instruction value found.

This effect can be used for several purposes:
  • Indexing of data, if C(K) doesn't cause the operand to overflow 12 bits.
  • Changing the instruction type, if the addition affects the top three bits of the instruction.
  • "Extending" a CS, TS, or AD instruction to an MP, DV, or SU instruction, if the addition causes the instruction value to overflow 15 bits.  This is the only manner in which the latter three instruction types can be triggered.

C(K) can be either positive or negative.


INHINT

Description:
"Inhibit interrupts"
Syntax:
INHINT
Operand(s):
None.
Timing:
2 MCT
Octal:
020017
Notes:
This instruction causes all interrupts to be inhibited until a RELINT instruction is executed.

It is actually a mnemonic for an "INDEX 17", but there is not actually any register at address 017, and the hardware treats this code specially rather than as an INDEX instruction.

MASK

Description:
"Mask"
Syntax:
MASK K
Operand(s):
K is any address in memory.
Timing:
2 MCT
Octal:
070000 + K
Notes:
This instruction takes the bitwise AND of the contents of a memory location and the accumulator:
C(A) = C(A) & C(K)
It does, however, have the side effect
C(K) = b(K)
which means that if K is an editing register, then it will be edited.

MP

Description:
"Multiply"
Syntax:
MP K
Operand(s):
K is any address in memory.
Timing:
8 MCT
Octal:
040000 + K
Notes:
This is an "extended" instruction, meaning that it is coded as
EXTEND
MP K
or by some operation such as
INDEX K0
MP K
that produces a 16-bit MP instruction value ... i.e., whose bit 16 is non-zero.  Thus even though the octal value of the instruction is shown above as 040000+K, and that's what appears in the rope and how the assembler sees it, in fact by the time it is executed it is really 0110000+K, which is how the CPU sees it.

This instruction multiplies two single-precision (i.e., 15-bit) values, from a memory location and the accumulator (sign-corrected), and produces a 29-bit value stored in the accumulator (more-significant word) and the LP register (less-significant word).  In other words, since the ranges of the input and output are each ±214, the range of the product must be just ±228, or 29 bits in all; the sign bit is duplicated into each of the two words, making a total of 30 bits.
C(A,LP) = b(A) × b(K)
The signs of the two output registers are identical, and are identical to the product of the signs of the two inputs ... which sounds obvious until you recognize that it covers cases like -0 × +53 = -0.

C(K) is unchanged, unless K is itself A or LP.

Note:  R-393, p. 3-7, says that this instruction take 10 MCT.  John Pultorak's simulator command-sequence simulator says that it takes 8, and for the present time, I accept what John says.

NOOP

Description:
"No-op"
Syntax:
NOOP
Operand(s):
None.
Timing:
2 MCT
Octal:
030000
Notes:
This instruction is a mnemonic for "XCH A", i.e., exchange the contents of the accumulator with itself.  Since that doesn't have any effect other than to use up a couple of MCT, it is a "no operation".

OVIND

Description:
"Overflow indicator (?)"
Syntax:
OVIND K
Operand(s):
K is any address in fixed memory.
Timing:
2 MCT if the accumulator contains no overflow, 3 MCT if the accumulator contains overflow.
Octal:
050000 + K
Notes:
This instruction is actually identical to TS, and is simply a different mnemonic for it that is less confusing when the operand is fixed memory, because when the operand is fixed memory it is impossible to copy the accumulator to the operand.  However, all other behavior (setting accumulator to 000001 or 177776 and skipping the next instruction on overflow) is identical to what has been described for TS.

OVSK

Description:
"Overflow skip"
Syntax:
OVSK
Operand(s):
None.
Timing:
2 MCT
Octal:
050000
Notes:
This instruction is a mnemonic for "TS A", though its behavior is not precisely identical to what you'd expect TS A to do, since C(A) is not modified even if there is overflow.

As you may expect, its action is to continue to the next address if the accumulator does not contain overflow, but skips the next address and proceeds to the address after that if the accumulator does contain overflow.

RELINT

Description:
"Release interrupts"
Syntax:
RELINT
Operand(s):
None.
Timing:
2 MCT
Octal:
020016
Notes:
This instruction causes all interrupts to be re-enabled after a corresponding a INHINT instruction has disabled them.

It is actually a mnemonic for an "INDEX 16", but there is not actually any register at address 016, and the hardware treats this code specially rather than as an INDEX instruction.

RESUME

Description:
"Resume" from interrupt
Syntax:
RESUME
Operand(s):
None.
Timing:
2 MCT
Octal:
020025
Notes:
This instruction is numerically equivalent to "INDEX 25", but is not an INDEX instruction.  As mentioned before, when an interrupt occurs, it automatically performs a sequence of steps like
Inhibit interrupts
C(BRUPT) = C(B)
C(QRUPT) = C(Q)
C(ZRUPT) = C(Z)
TC to interrupt-service routine
where (recall) B is the register that holds next instruction that would have been executed when the interrupt occurred.  (Not necessarily C(L), since an INDEX instruction might have preceded it an altered the numerical value of the instruction.)  Note that this interrupt inhibition is a different mechanism from the one used by INHINT and RELINT.

What RESUME does is to undo these steps:
C(B) = C(BRUPT)
C(Q) = C(QRUPT)
C(Z) = C(ZRUPT)
Stop inhibiting interrupts
This has the effect of putting the program counter (Z) back to what it had been before the interrupt, restoring any return address that had been in Q, and executing the same instruction (numerically) that had been about to execute, regardless of whether it's what was stored at the return location or not: i.e., regardless of whether or not the interrupt had occurred between an INDEX instruction and the instruction following it.

Notice that in theory, you could force any instruction you like to execute upon return from interrupt, simply by replacing the contents of the BRUPT register from within the interrupt-service routine.  Why you might want to do that, I can't say.

RETURN

Description:
"Return"
Syntax:
RETURN
Operand(s):
None.
Timing:
1 MCT
Octal:
000001
Notes:
This instruction is a mnemonic for "TC Q", meaning that it can be used to return from a subroutine.

SQUARE

Description:
"Square"
Syntax:
SQUARE
Operand(s):
None.
Timing:
8 MCT
Octal:
040000
Notes:
This is an "extended" instruction, meaning that it is coded as
EXTEND
SQUARE
Thus even though the octal value of the instruction is shown above as 040000, and that's what appears in the rope and how the assembler sees it, in fact by the time it is executed it is really 0110000, which is how the CPU sees it.

This instruction has the effect
C(A,LP) = b(A) × b(A)
and all of the comments for MP apply to it.

SU

Description:
"Subtract"
Syntax:
SU K
Operand(s):
K is any address in memory.
Timing:
2 MCT or 3 MCT
Octal:
060000 + K
Notes:
This is an "extended" instruction, meaning that it is coded as
EXTEND
SU K
or by some operation such as
INDEX K0
SU K
that produces a 16-bit SU instruction value ... i.e., whose bit 16 is non-zero.  Thus even though the octal value of the instruction is shown above as 060000+K, and that's what appears in the rope and how the assembler sees it, in fact by the time it is executed it is really 0130000+K, which is how the CPU sees it.

This instruction subtracts the contents of a memory location from the accumulator:
C(A) = C(A) - C(K)
In all other respects — timing, side-effects, special cases — it is identical to the AD instruction.

TCAA

Description:
"Transfer control to address in A"
Syntax:
TCAA
Operand(s):
None.
Timing:
2 MCT
Octal:
050002
Notes:
This instruction is a mnemonic for "TS Z", though its behavior is not precisely identical to what you'd expect TS Z to do, since there is no skip-on-overflow.

Suppose that the initial contents of the accumulator, b(A), is the logical OR
b(A) = OP | K
where only the 4 most-significant bits of the 16-bit value OP may be non-zero, and only the least-significant 12 bits of K may be zero.  The operation of TCAA will be:
  • C(A):
    • If b(A) contains no overflow: C(A)=b(A).
    • If b(A) contains positive overflow: C(A)=000001.
    • If b(A) contains negative overflow: C(A)=177776.
  • The next instruction executed will be at address K.

But there's a tricky aspect to this, in that since TCAA is still a "transfer to storage" operation, this means that the 16-bit Z register will in fact have its upper 4 bits loaded with OP, and those upper 4 bits remain set unless you explicitly set them to something else!  In other words, the lower 12 bits of Z will continue to change as we advance from one instruction to the next, but the upper 12 bits won't change. However, the upper 4 bits of the Z register are normally 0, and if OP isn't zero, that leaves a potential problem lurking for the future.  The problem is what happens when the next TC instruction is encountered.  Recall that a TC instruction, in addition to transferring control, also loads the Q register with the return address.  Now, that's a shorthand way of saying that Q gets loaded with a TC to the return address.  But if OP isn't zero, then what that eventual TC loads into Q is not a TC to the return address, but some other instruction (OP) whose operand is the return address.  Of course, a TC which is a simple "jump" won't have a problem, since it won't expect to find any return address, and the problem will occur only if you're using it as a call to a subroutine.

All of which boils down to saying that unless you intend to exploit this wacky feature, don't use this instruction, or else make sure you get the upper 4 bits of Z set back to zero somehow before the next subroutine call you want to use!

TC or TCR

Description:
"Transfer Control"
Syntax:
TC K
Operand(s):
K is any address whatever in memory.  If less than 06000 it is in erasable or fixed-fixed memory, while if in the range 06000 to 07777 is in banked fixed memory and the Bank register is used to determine the applicable memory bank.  Sometimes the TC occurs then Bank holds 00000, which is actually interpreted as bank 03.
Timing:
1 MCT
Octal:
000000 + K
Notes:
This is used both for unconditional jumps to locations, or for calling subroutines.  It can be done for the latter because a side effect is that
C(Q) = L + 1
i.e., that the Q register is loaded with the next address following the TC instruction (and the original value of Q is lost), and a return from a subroutine can be done with the instruction
TC Q
But there's no stack, so you have to be extremely careful when doing things like calling subroutines from within other subroutines, because each call destroys the existing return address.  So one thing that subroutines typically do is to save the Q register as a variable immediately upon entry , and to restore it from that variable immediately prior to exiting.

The instruction TCR does not differ from TC in any way, but it may clarify the intention of your source code to use TCR when you are calling a subroutine from which there will be a return, and TC when you are performing a simple jump.  However, this seems to have been done very seldom in a program like Solarium.

Note that a return from interrupt is not done in this manner, and requires its own dedicated instruction, RESUME.

TS

Description:
"Transfer to Storage"
Syntax:
TS K
Operand(s):
K is any address in erasable memory (0-01777).
Timing:
2 MCT if the accumulator contains no overflow, 3 MCT if the accumulator contains overflow.
Octal:
050000 + K
Notes:
This instruction always copies the accumulator to memory,
C(K) = C(A)
If K is 15-bit memory, then A is sign-corrected (i.e, the 16th bit US is moved to the 15th bit SG) before storing.  If K is an editing register, then editing is performed during storage.

Skip on Overflow

If the accumulator does not contain overflow, then that is the end of the operation.  But if the accumulator does contain overflow, then the following "skip on overflow" operation (which occupies an additional 1 MCT) is performed:
  • If b(A) contains positive overflow, then C(A)=000001.
  • If b(A) contains negative overflow, then C(A)=0177776.
  • The instruction at L+1 is skipped, and the next instruction executed is at L+2.
This skip-on-overflow feature is used for multi-precision arithmetic, where it is convenient, but it means that the TS instruction has to be used with extreme caution in other circumstances.  If you think of it merely as a storage instruction, you will quickly run into circumstances where it's behavior is very confusing.

XAQ

Description:
"Execute C(A) using Q"
Syntax:
XAQ
Operand(s):
None.
Timing:
1 MCT
Octal:
000000
Notes:
This instruction is a mnemonic for "TC A", meaning that it will:
  • Jump to address 0, storing a return address in Q.
  • Execute whatever instruction it finds at address 0 (which is the A register).
  • Proceed to address 1 (presuming that there wasn't a TC or CCS at address 0).
  • Since what is stored at address 1, the Q register, is the return address, which is numerically identical to a TC to the return address, it will thus return to the address following the XAQ.
However, this is confusing when you see it in a simulation, and R-393 recommends instead using the following presumably less-confusing commands in preference to an XAQ:
INDEX A
TC 0

XCH

Description:
"Exchange"
Syntax:
XCH K
Operand(s):
K is any address in erasable memory (0-01777).
Timing:
2 MCT
Octal:
030000 + K
Notes:
This instruction exchanges C(A) and C(K).  If K is an editing register, it is edited in the process of doing this.

The opcode is numerically identical to the CAF instructions, with the difference being that K is in erasable rather than fixed memory.

Note:  The Virtual AGC Block I simulator will not change C(K) if K happens to be one of the input registers, IN0 - IN3.


Pseudo-Operations

The pseudo-ops are a subset of those in Block II.  Actually, yaYUL supports the identical pseudo-ops for Block I as it does for Block II, but some of those pseudo-ops simply make no sense for Block I and therefore will never appear in actual code.  I know I should have yaYUL exclude the nonsensical pseudo-ops, but I have no present intention of doing so.  See the Block II description.

Interpreter Instruction Set

Block I interpreter language is superficially similar to Block II interpreter language, but is actually structured quite differently.  Moreover, it partakes of certain coding conventions not present in Block II.  It is also missing a number of interpreter commands that are present in Block II, while it has a number of commands that are not present in Block II.

Source Code and Encoding

Interpreter source code is structured as a series of what are referred to as "equations", though they are not.  Each "equation" consists of a group of commands of variable length, followed by a group of operands of a variable length.

There are several different forms an equation can take, and rather than trying to give you a rule for them, I'll just illustrate the 4 possible forms they can take:
# Pattern 1:
OPERATOR
            OPERAND1
            .
            .
            .
            OPERANDN

# Pattern 2:
OPERATOR
A   OPERATORB
            OPERAND1
            .
            .
            .
            OPERANDN

# Pattern 3:
OPERATOR
0   M
OPERATOR1A  OPERATOR1B
.
.
.          
OPERATORMA  OPERATORMB
            OPERAND1
            .
            .
            .
            OPERANDN


# Pattern 4:
OPERATOR
0   M
OPERATOR1A  OPERATOR1B
.
.
.          
OPERATORM
            OPERAND1
            .
            .
            .
            OPERANDN
Now, each operator employs a certain number of operands, either 0 or 1, and you would superficially expect the number of operands in the equation to add up to the number of operands required by the operators.  However, this is seldom true, and there can be either more or less operands than you would expect.

TBD


Control-Pulse Sequences

As has been explained above, the Block I AGC's "basic instructions" (i.e., the assembly-language instructions as opposed to interpretive instruction) mostly require 2 machine cycle times (MCTs) to executed, although the TS instruction usually takes only 1 MCT, and others like MP or DV take considerably more.  One MCT requires about 11.7 μs, or more-precisely, 12/1.024 = 11.71875  μs (plus or minus whatever the clock tolerance is, of course).

That is the viewpoint from the abstraction level of "basic instructions", and is the world-view enforced by our Block I CPU simulator, but does not represent the underlying physical reality of hardware AGC.  From the physical standpoint:

The sequence of control pulses corresponding to a basic instruction is, of course, its "control-pulse sequence".  In theory, any question about the ultimate behavior of any given basic instruction can be answered by analyzing its control-pulse sequence closely enough, although this can be quite a challenging proposition, particularly for complex instructions like MP or DV.  For example, when the DV instruction was defined earlier, certain constraints were placed on the dividend vs the divisor, and if those constraints weren't satisfied, we merely stated that the results were undefined.  However, they're not undefined, and you can find out what the result should be if you analyze the control-pulse sequences.  However, CPU simulator does not do that, and you cannot expect agreement with the physical AGC in those cases.  Of course, the danger is that original AGC developers could have used their inside knowledge of what should have happened, rather than abide by the documented constraints, and hard-coded that tribal knowledge into a program like Solarium.  Well, if they did, then it will make me sad.

Control-pulse sequences are used for more than just basic instructions, however.  All manner of auxiliary operations are coded as control-pulse sequences, and thus occupy CPU time when they occur.  These include:

My focus in this project is to provide useful software simulation of the AGC and so, while I consider simulation of the control-pulse sequences to be the technically "correct" way of creating such a simulation, I also believe that reaching the point of having a satisfactory practical understanding of control-pulse sequences has a far-steeper learning curve than obtaining a practical understanding of basic AGC assembly-language programming.  Moreover, programming the basic instructions much have been what AGC developers did 99% of the time, with teasing out control-pulse sequences (or asking an on-site expert about them) must have represented very little of their time.  So from that standpoint, I consider simulating the basic instructions themselves, and ignoring control-pulse sequences, to be the "correct" overall approach.  Your opinion may, of course differ.  Plus, it never occurred to me to do it that way.

The only knowledge of control-pulse sequences you need in order to follow the remainder of the discussion on the present page is that the control-pulse sequence that increments a CPU counter register is called a PINC, and one which decrements it is called a MINC.

If you do want to find out more about control-pulse sequences in the Block I AGC, the discussion of them (intermixed with discussion of basic instructions) is spread throughout Chapter 3 of R-393.


Available Block I AGC Software

At present, the only true Block I programs available are:

See also the section on John Pultorak's assembler and simulator.


Available Supporting Software

Virtual AGC's Assembler (yaYUL)

The Virtual AGC project itself also provides a Block I assembler, and it is the same yaYUL assembler used for Block II code.  The only difference is that you add a command-line switch of --block1, but otherwise it operates identically, and accepts the full syntax of the Solarium program.

CPU Simulators

Comparison

There are two Block I CPU simulators.  Because each has its advantages, both are described in more detail in the sections dedicated to them that follow.  However, a capsule comparison is given by the following table. 

Feature
Pultorak Simulator (yaAGC-Block1)
Virtual AGC Simulator (yaAGCb1)
Detailed information
See the next section
See second section after this
Design rationale
Simulates command-pulse sequences
Simulates basic instruction set
DSKY?
Textual interface only
Operates with the simulated DSKY
Uplink?
No
Operates with the simulated uplink.
Other peripherals?
Text-based interface
Has a yaAGC-type socket interface or (theoretically) NASSP/Orbiter interface for implementation of arbitrary peripheral devices
Language
C++
C
Building the simulator
Any platform supporting gcc or similar
Any platform supporting gcc or similar
Written by
John Pultorak
Ron Burkey
Purpose
Intended to support John's development of his hardware Block I simulator, running John's port of a portion of the Block II program Colossus 249.
Intended to intended to integrate into Virtual AGC on the same footing as Block II AGC and AEA simulators, and specifically to run Solarium 055.
Status
Fairly usable.
Progressing nicely, but not quite as mature as the Pultorak simulator yet.

The table above refers to the version of John Pultorak's simulator which has been ported to gcc and corrected, rather than to his original code, which is also available.  Both versions are discussed in the following section.

John Pultorak's Assembler and Simulator

Preliminary to his construction project for a hardware simulation of the Block I AGC, or even the existence of the Virtual AGC project at all, John Pultorak also developed a Block I AGC assembler and Block I AGC software CPU simulator as a tool in aiding his development of his hardware simulation.  The assembler accepts only John's own syntax rather than actual Block I program syntax, based on manual entry and editing of source code (for example, I believe it does not accept Block I interpreter code), and I have nothing further to say about it.  Editing a 1000-page program for use with it would be overwhelming, particularly when there's an alternate assembler (yaYUL) that already accepts the full syntax.  Rather, my scope here is limited to the simulator.

John's original software source code for the simulator, intended to be built with Microsoft Visual C++, is available from us.  Unfortunately, his source-code files only cover his simulator versions through 1.15.  Nevertheless, I have extracted version 1.16 from the program listing in his PDF description, and it is contained in the Pultorak-Simulator-1.16/ directory of our GitHub repository.

Donna Polehn has also created a kind of Visual C++ assembler/simulator development environment based on this original code, in so far as I understand it, which you may find interesting. 

Since I don't myself use Visual C++, or even Windows if I can help it, John's Visual C++ source code was of no direct use to me.  I have, however, taken the steps needed to port version 1.16 of John's simulator to GNU gcc (g++).  Feel free to assume that any deficiencies in the user interface are due my porting effort, and it's certainly true that I "fixed" things in his program that I later had to "fix" back to what John had originally.  It's perhaps worth noting that my purpose in porting this program was primarily to use it as a comparison and sanity check against my own simulator, as described in the next section, and so my motivation in improving the program's user interface (assuming it needs improvement) was lacking.  Somebody might find pepping up John's original source or my gcc port of it to be an interesting exercise.  I, however, personally decline this opportunity for fun.

Right now, you can find this ported code in our GitHub repository.  I have only worked with it in Linux, but I expect it should probably build in Mac OS X or Windows (with MinGW/Msys), as long as you have g++ and pthreads installed.  All you have to do is
cd DirectoryContainingTheSource
make
The program defaults to loading Solarium055, for which you should have Solarium055.bin and Solarium055.lst, and hopefully Solarium055.pad, or at least symbolic filesystem links to them, in the current directory.  The command to run it is simply
./yaAGC-Block1 --power
at which point anything else that happens must be controlled by the program's internal textual interface.  John describes using this command set in his PDF description of the simulator, though my own changes have forced changes in the command set as well.  The commands I personally find useful are:

However, this is not necessarily a complete list, even of the commands I created for it, so please do use the 'm' command to see what additional ones there may be that I've forgotten to list here.  There are also commands for John's built-in textual DSKY, but I don't understand how they work, and I have only used the simulator essentially without a DSKY.

There are also command-line options that allow you to do various things, such as selecting a different program than Solarium 055.  The program will accept rope files and program-listing files created either yaYUL (with the --block1 switch), assuming you had some Block I program other than Solarium to work with, or else as produced by John's own assembler.  A yaYUL command like the following

yaYUL --block1 --unpound-page MAIN.agc >program.lst
mv MAIN.agc.bin program.bin
would produce the necessary files, which could then be run in the simulator as follows:

./yaAGC-Block1 --power --rope=program

As far as John's own sample Block I program (agc.bin + agc.lst), which he manufactured manually from portions of Colossus 249, it will actually no longer run properly in this ported version of the simulator, even though the simulator accepts output from John's assembler.  JThat would require the use of John's original Visual C++ code.

The reason for this is that the program has not merely been ported from Visual C++ to gcc, but also corrected in a variety of ways, and these corrections prevent John's original code from running, although the changes needed to make it run seem fairly trivial.  The reason that the corrections were needed do not reflect on John, or on anybody, but are just an unfortunate fact of life.  Specifically, at the time John created his project, the principal (only?) written documentation he had to work from was Instrumentation Labs document R-393, which was itself inaccurate in a number of ways.  As the document itself points out in its Preface,
"... Fine detail and internal consistency have been under-emphasized for the sake of promptness so that this report could be written within a few weeks of the inception of the design."
In other words, they had to get it done and get it into service quickly, and didn't have time fix every little thing in it.  Moreover, there was no available sample of Block I software of any kind for John to work with.  In fact, as he himself says, the sole sample of AGC code he had, the Block II program Colossus 249, was itself not complete, and was merely a fragment.  So all things considered, it is remarkable that he got any of it to work at all, and the fact that there are some errors is inevitable.  But those errors are more than enough to prevent John's original code from running on a corrected version of his simulator.

The reason I am pointing this out is to provide you with a warning, should you decide to forego the corrected, gcc version of the program, and instead revert to John's original Visual C++ simulator.  None of the corrections for the problems I've been mentioning have been back-ported to the Visual C++ version of the program.  It might be an interesting exercise for somebody to indeed backport these changes.  The most-significant problems were:
  1. The memory model is undersized:  the amount of fixed rope memory in the device was increased after R-393 was written, from the 12 banks to 24 banks, and Solarium 055 will in fact not fit into 12 banks.
  2. The (corrected) interrupt-vector table is at address 2000, and the entry point for the program is at 2030.  In the original version of the program, however, they are at 2004 and 2000, respectively.
  3. Timer registers (TIME1, 2, 3, and 4) increment at 10× the speed they're supposed to. Specifically, TIME1, 3, and 4, which are supposed to increment every 10 ms., actually increment every 1 ms. TIME2, which is triggered by overflow in TIME1, increments every 16.384 seconds rather than every 163.84 seconds as it's supposed to.
  4. Okay, I admit I'm not too sure about this one ... but the sim seems to integrate parity bits everywhere.  That gave me a lot of trouble, so I simply disabled it.
  5. Bit assignments in output-register OUT1 (only OUT0-OUT1, of OUT0-OUT4 are implemented) are not correct. They unfortunately had to be taken from the bit assignments of the Block II output register of the same name, but those do not correspond to the Block I computers. (The corresponding OUT0 registers in Block I and Block II do, however, correspond perfectly to each other!)
A remarkably short list of problems, but nevertheless a list in which one would encounter difficulties immediately in trying to run actual Block I software ... as indeed I did. 

Here is the full syntax at present for using the gcc port of John's simulator:
yaAGC-Block1 [OPTIONS]
where the available options are:

Virtual AGC's CPU Simulator (yaAGCb1)

My own Block I simulator is written independently of John Pultorak's, and no code from John's has been reused in mine, nor served as a model for mine.  That isn't intended to imply that John's program was not used, or that there is great flaw that prevents it from being used.  In fact, I used it extensively as a cross-check on the functioning of mine, with the intention of being able to run the two side-by-side, and have them match up register-for-register, instruction-for-instruction, on a cycle-by-cycle basis.  Sometimes this revealed errors in John's simulator, which I corrected.  Other times, it revealed bugs in mine, which I corrected.  Often, there were just differences I hadn't anticipated, usually involving arithmetical overflow bits that got written into registers I hadn't expected; in which case, when they were reasonable even if unexpected, I did what checking I could but almost always adopted John's approach in place of my own.

So the upshot of that is that these programs now behave essentially identically.

Then why have two (other than the obvious advantage of being able to cross-check one against the other ... though one shouldn't underestimate the great advantage of being able to do that)?  Well, it mainly has to do with the fact that the CPU simulator has to be able to integrate with other Virtual-AGC style peripheral devices, such as simulated DSKYs, to be able to participate in the GUI code::blocks style debugging capabilities that other Virtual AGC simulators have, and so on, and after investigating it I just thought it was cleaner and simpler to start from scratch in doing so, given the programming style I personally preferred to use.  Obviously, others' opinions may differ, and the problems I perceived I was solving could easily be more in my mind than in John's program.

You can find code for my new simulator in our GitHub repository.  I have only worked with it in Linux, but I expect it should probably build in Mac OS X or Windows (with MinGW/Msys), as long as you have g++ and pthreads installed.  All you have to do is

cd DirectoryContainingTheSource
make
The program defaults to loading Solarium055, for which you should have Solarium055.bin and Solarium055.lst, and preferably Solarium055.pad as well, or at least symbolic filesystem links to them, in the current directory.  The command to run it is simply
./yaAGCb1
at which point anything else that happens must be controlled by the program's primitive textual-debugging interface, the simulated DSKY interface, or the simulated digital uplink.  The program's textual debugging interface is indeed extremely primitive.  The only existing commands at the moment are:
One useful capability that both of the CPU simulators (Pultorak and Virtual AGC) have is to be able to produce a log file in identical formats of the cycle-by-cycle program execution.  This allows easy comparison for discrepancies with programs like diff or meld, or any of a number of others.  The steps in either simulator are the same:
  1. Run the simulator with a command-line switch "--log=FILENAME".
  2. Execute identical portions of the code in the simulator, for example with "t2000" to execute 2000 assembly-language instructions.
  3. Quit the simulator ("q").

This capability is enhanced with the 'bcN' and 'l' commands, since those may allow you to avoid adding a large amount of information to the log when you know in advance that it will be identical.

Here is the full syntax at present for using the my Block I simulator is:

yaAGCb1 [OPTIONS]
where the available options are:

Status of yaAGCb1

I have not fully completed yaAGCb1 in the sense that yaAGC is complete, and thus wouldn't expect it to fully work if integrated into a full spacecraft simulator.  While I don't have a complete list at the moment of what works and what doesn't, nor have all the parts of yaAGCb1 that I think work been fully tested, I can definitely say that I've not yet bothered with the following:

Virtual AGC's DSKY Simulator (yaDSKYb1)

There are two versions of the simulated DSKY, corresponding to the control-panel and nav-bay versions of the physical DSKY as described earlier, but both are available from the same yaDSKYb1 program, with different command-line options.  The code resides in the same yaDSKYb1/ directory in our GitHub repository.

Building this software is simply a matter of cd'ing into its source directory and running 'make'.   There are a number of graphical images which the program needs to use as resources in order to work properly, and by default these are found in the images/ sub-directory of the same directory in which yaDSKYb1 is being run from, and finding these images is likely the principal problem the program will have in trying to run, but you can specify the directory on the command line:
cd ParentDirectoryOfyaDSKYb1/
yaDSKYb1/yaDSKYb1main [--images=DIRECTORY] [--port=PORTNUM] [--nav-bay]
The value for PORTNUM depends on the range of TCP ports on which yaAGCb1 is listening, but the default value of 19671 is usually satisfactory.

Unlike the Block II AGC, there are not separate i/o ports (i.e., INn and OUTn registers) in the AGC for the control-panel and nav-bay DSKYs, so I'm not sure how the Block I AGC connected to more than one DSKY at a time.

Virtual AGC's Digital Uplink Simulator (yaUplinkBlock1)

At present, a program called yaUplinkBlock1 is provided (in the similarly-named source-code directory in our GitHub repository. It is a simple command-line program, in which you can type (or feed in from a script) ASCII mnemonics for DSKY keys, which the program then converts to the proper uplink format and sends to the Block I AGC simulator.

The ASCII mnemonics for the various DSKY keys, rather straightforwardly, are:

Thus, entering "v36<Enter>" in yaUplinkBlock1 is equivalent to V36E on the DSKY keypad.

The full command-line syntax is

yaUplinkBlock1 [--port=PORTNUM] [--batch]

The --port setting, of course, changes the default TCP port (19675) of the uplink program.  By default, yaUplinkBlock1 is suitable for accepting input interactively from a computer keyboard, but not from a (say) a script.  The --batch switch flips that around, so that (for example) with the --batch switch you could do something like the following if you wanted to:

echo "v11n16" | yaUplinkBlock1 --batch

Taking Solarium for a Spin

At the time I'm writing this, the Block I simulation is still in a pretty primitive state, and undoubtedly rife with bugs, but if you're really keen on trying bleeding-edge stuff, there are some things you can do with it. 

If you have a version of the VirtualAGC GUI that's new enough to have support for Solarium, you can run it by selecting Apollo 6 in the GUI. 

If not, you have to at least have built the virtualagc source tree.  You then need to run the AGC and DSKY simulators separately, as follows, probably from two separate command lines; use the --nav-bay, without the brackets shown below, if you want to use the navigational-bay version of the DSKY, but by default you'll get the main control-panel version of the DSKY:
cd PathToVirtualagcSourceTree/yaDSKYb1
./yaDSKYb1 [--nav-bay]
and
# Start the AGC.
cd PathToVirtualagcSourceTree/yaAGCb1
# Make sure that Solarium is available easily to the simulator.  Actually, the following
# instruction works as shown only in Linux.  In Mac OS X, I think the switch "--symbolic"
# is probably something else (like -S, perhaps), and in Windows you can't make a symbolic
# link like this at all, and will simply have to copy the files Solarium055.bin, .lst, and .pad
# into this directory.
ln --symbolic ../Solarium055/Solarium055.{bin,lst,pad} .
./yaAGCb1 --run

From this point, you can now interact with the AGC, running Solarium, entirely through the DSKY.  There is kind of a dilemma, though, in that the references for the kinds of things you can do with Solarium are pretty sparse, or at least haven't yet reached me.  You have a few choices, if you want to explore them on your own:
  1. R-467, The Compleat Sunrise briefly covers what was available in the Block I SUNRISE program (September 1964). 
  2. You can pick through the Solarium 055 source code (April 1968), to try and figure out what's available.
  3. You can look at the available documentation for Colossus 237 (December 1968), though considering that Colossus 237 was a Block II program and Solarium a Block I program, it's unclear how much similarity we can expect to see.
Unfortunately you can't get useful Solarium-related information from John Pultorak's meticulously-crafted Block I documents and demonstration ... the problem being, you see, that John had no Block I software to use as a model, and hence based his Block I hardware simulation on Block II AGC software, namely Colossus 249, which is later even than Colossus 237.  But your mileage may vary, and it doesn't hurt to look if you like.  As a practical option I fear that choice number 2 (picking through the Solarium source code) is really the best place to start at the present time.

But anyway, assuming you have started the simulation as indicated above, I do know enough to tell you how to do a few things with it:

Click to enlarge
Startup screen, immediately after starting simulation.
Actually, this is not really the first thing you see, but just the first screen that persists long enough to take a screenshot of it. 

At first, it will really show "PROGRAM 00" rather than "PROGRAM 77", because the AGC is in "major mode" 00.  What has happened, however, is that on power-up the AGC hasn't been able to detect any Inertial Measurement Unit (IMU), because we don't have a simulation for one hooked up to it!  Detecting this condition, a specific AGC program called the "Night Watchman" has detected this condition and decided to flip over to major mode 77 ... which isn't documented, as far as I can tell, and none of the original AGC developers I've contacted remember it, including Jim Kernan, who was Solarium's "rope mother".

Of the other items displayed, "VERB 05" is an "octal display of data" while "NOUN 31" indicates that the data being displayed is "Failreg", the failure register.  The 5-digit displays, I believe, are the last three error conditions reported, of which only one, 00203 actually has an error code in it.  Thus, you are seeing "Alarm 00203".  According to the source code, alarm 00203 is "NO IMU MODE INDICATED TO COMPUTER".

The IMU mode is communicated to the AGC through its input register IN2, I believe, which is all zeroes at this point, given that there is no IMU, and all zeroes is not recognized as a legitimate IMU mode.

Click to enlarge
V36E
No problem.  Let's use V36E, "Fresh Start".  It doesn't get rid of the Alarm 00203 message, but at least it does put us into major mode 00, as we're entitled, I expect.

Click to enlarge
V32EEE I don't actually know how to get rid of that Failreg display, short of instructing the AGC to display something else ... or we could use V32E, "Bump displays", i.e., scroll the register display downward.  To get rid of all 3 error codes, we have to do it three times.

Click to enlarge
V31N02E
We could use V32N02E to let us display the contents of the AGC's memory.  What you see if you use this command is that the "REGISTER 3" display clears, and we can enter an octal address.  These addresses are what I personally call "flat" addresses, though I think there may be some official buzzword for it that I don't recall at the moment.  With flat addresses, the entire AGC memory space is simply a continuous one from octal addresses 000000 through 071777, where
  • 000000-001777 is erasable memory.
  • 002000-005777 are "fixed-fixed" memory.
  • 006000-007777 is bank 03
  • 010000-011777 is bank 04
  • ...
  • 070000-071777 is bank 34.

So if, for example, I now entered 12345E (into the open space for REGISTER 3), what I should get is the contents of 05,6345, which a quick check of Solarium's assembly listing reveals to be 03136.  And amazingly, that's what the DSKY shows in REGISTER 1 as well.

At this point, you can actually keep examining as many memory locations as you like, just by pressing ENTER, then a new octal address, and then ENTER again.  It doesn't seem to work for registers, though.  Perhaps the address should be kept at 060 or higher.


Click to enlarge
V16N65E
Or perhaps, we might want to display the time since startup.  V16, " Monitor (in decimal) all component (s) of", combined with N65E, "Time (Hours and Seconds)", does the trick. 

The terse descriptions of the verbs and nouns from resources like R-467 make it a bit tough to figure out what we're actually seeing on the DSKY's display, but you can figure it out with a little bit of cogitation:
  • REGISTER 1:  The time, in decimal, in units of 1/100 hours.  Therefore, it increments every 3600/100=36 seconds.
  • REGISTER 2:  The time, in decimal, in units of 1/100 seconds.  According to R-393, it should be updating every 1/2 second, but it's pretty clear that it's updating once per second instead.   Since it only goes up to +99999, obviously we expect it to wrap around to +00000 every 1000 seconds.





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