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Proof INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.acg #592 (#708)

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Co-authored-by: James Harris <wopian@wopian.me>
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panoreak 2020-10-10 22:01:06 -04:00 committed by GitHub
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61
Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.agc
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@ -26,31 +26,31 @@
# Page 54 # Page 54
# *** CHANNEL DESCRIPTION WORDS ARE ALLOCATED IN ERASABLE ASSIGNMENTS *** # *** CHANNEL DESCRIPTIONSF WORDS ARE ALLOCATED IN ERASABLE ASSIGNMENTS ***
# CHANNEL 1 IDENTICAL TO COMPUTER REGISTER L (0001) # CHANNEL 1 IDENTICAL TO COMPUTER REGISTER L (0001)
# CHANNEL 2 IDENTICAL TO COMPUTER REGISTER Q (0002) # CHANNEL 2 IDENTICAL TO COMPUTER REGISTER Q (0002)
# CHANNEL 3 HISCALAR: INPUT CHANNEL; MOST SIGNIFICANT 14 BITS FROM 33 STAGE BINARY COUNTER. SCALE # CHANNEL 3 HISCALAR; INPUT CHANNEL; MOST SIGNIFICANT 14 BITS FROM 33 STAGE BINARY COUNTER. SCALE
# FACTOR IS B23 IN CSEC, SO MAX VALUE ABOUT 23.3 HOURS AND LEAST SIGNIFICANT BIT 5.12 SECS. # FACTOR IS B23 IN CSEC, SO MAX VALUE ABOUT 23.3 HOURS AND LEAST SIGNIFICANT BIT 5.12 SECS.
# CHANNEL 4 LOSCALAR: INPUT CHANNEL; NEXT MOST SIGNIFICANT 14 BITS FROM THE 33 STAGE BINARY COUNTER # CHANNEL 4 LOSCALAR; INPUT CHANNEL; NEXT MOST SIGNIFICANT 14 BITS FROM THE 33 STAGE BINARY COUNTER
# ASSOCIATED WITH CHANNEL 3. SCALE FACTOR IS B9 IN CSEC. SO MAX VAL IS 5.12 SEC AND LEAST # ASSOCIATED WITH CHANNEL 3. SCALE FACTOR IS B9 IN CSEC. SO MAX VAL IS 5.12 SEC AND LEAST
# SIGNIFICANT BIT IS 1/3200 SEC. SCALE FACTOR OF D.P. WORD WITH CHANNEL 3 IS B23 CSEC. # SIGNIFICANT BIT IS 1/3200 SEC. SCALE FACTOR OF D.P. WORD WITH CHANNEL 3 IS B23 CSEC.
# CHANNEL 5 PYJETS: OUTPUT CHANNEL; PITCH RCS JET CONTROL. (REACTION CONTROL SYSTEM) USES BITS 1-8. # CHANNEL 5 PYJETS; OUTPUT CHANNEL; PITCH RCS JET CONTROL. (REACTION CONTROL SYSTEM) USES BITS 1-8.
# CHANNEL 6 ROLLJETS: OUTPUT CHANNEL; ROLL RCS JET CONTROL. (REACTION CONTROL SYSTEM) USES BIT 1-8. # CHANNEL 6 ROLLJETS; OUTPUT CHANNEL; ROLL RCS JET CONTROL. (REACTION CONTROL SYSTEM) USES BIT 1-8.
# CHANNEL 7 SUPERBNK: OUTPUT CHANNEL; NOT RESET BY RESTART; FIXED EXTENSION BITS USED TO SELECT THE # CHANNEL 7 SUPERBNK; OUTPUT CHANNEL; NOT RESET BY RESTART; FIXED EXTENSION BITS USED TO SELECT THE
# APPROPRIATE FIXED MEMORY BANK IF FBANK IS 30 OCTAL OR MORE. USES BITS 5-7. # APPROPRIATE FIXED MEMORY BANK IF FBANK IS 30 OCTAL OR MORE. USES BITS 5-7.
# CHANNEL 10 OUT0: OUTPUT CHANNEL; REGISTER USED TO TRANSMIT LATCHING-RELAY DRIVING INFORMATION FOR # CHANNEL 10 OUT0; OUTPUT CHANNEL; REGISTER USED TO TRANSMIT LATCHING-RELAY DRIVING INFORMATION FOR
# THE DISPLAY SYSTEM. BITS 15-12 ARE SET TO THE ROW NUMBER (1-14 OCTAL) OF THE RELAY TO BE # THE DISPLAY SYSTEM. BITS 15-12 ARE SET TO THE ROW NUMBER (1-14 OCTAL) OF THE RELAY TO BE
# CHANGED AND BITS 11-1 CONTAIN THE REQUIRED SETTINGS FOR THE RELAYS IN THE ROW. # CHANGED AND BITS 11-1 CONTAIN THE REQUIRED SETTINGS FOR THE RELAYS IN THE ROW.
# CHANNEL 11 DSALMOUT: OUTPUT CHANNEL; REGISTER WHOSE BITS ARE USED FOR ENGINE ON-OFF CONTROL AND TO # CHANNEL 11 DSALMOUT; OUTPUT CHANNEL; REGISTER WHOSE BITS ARE USED FOR ENGINE ON-OFF CONTROL AND TO
# DRIVE INDIVIDUAL INDICATORS OF THE DISPLAY SYSTEM. BITS 1-7 ARE A RELAYS. # DRIVE INDIVIDUAL INDICATORS OF THE DISPLAY SYSTEM. BITS 1-7 ARE A RELAYS.
# #
# BIT 1 ISS WARNING # BIT 1 ISS WARNING
@ -70,7 +70,7 @@
# BIT 14 ENGINE OFF # BIT 14 ENGINE OFF
# BIT 15 SPARE # BIT 15 SPARE
# CHANNEL 12 CHAN12: OUTPUT CHANNEL; BITS USED TO DRIVE NAVIGATION AND SPACECRAFT HARDWARE. # CHANNEL 12 CHAN12; OUTPUT CHANNEL; BITS USED TO DRIVE NAVIGATION AND SPAECRAFT HARDWARE
# #
# BIT 1 ZERO RR CDU; CDU'S GIVE RRADAR INFORMATION FOR LM # BIT 1 ZERO RR CDU; CDU'S GIVE RRADAR INFORMATION FOR LM
# BIT 2 ENABLE CDU RADAR ERROR COUNTERS # BIT 2 ENABLE CDU RADAR ERROR COUNTERS
@ -85,11 +85,11 @@
# BIT 11 -ROLL GIMBAL TRIM (BELL MOTION) DESCENT ENGINE # BIT 11 -ROLL GIMBAL TRIM (BELL MOTION) DESCENT ENGINE
# BIT 12 +ROLL GIMBAL TRIM (BELL MOTION) DESCENT ENGINE # BIT 12 +ROLL GIMBAL TRIM (BELL MOTION) DESCENT ENGINE
# BIT 13 LR POSITION 2 COMMAND # BIT 13 LR POSITION 2 COMMAND
# BIT 14 ENABLE RENDEZVOUS RADAR LOCK-ON; AUTO ANGLE TRACK'G # BIT 14 ENABLE RENDESVOUS RADAR LOCK-ON;AUTO ANGLE TRACK'G
# BIT 15 ISS TURN ON DELAY COMPLETE # BIT 15 ISS TURN ON DELAY COMPLETE
# Page 56 # Page 56
# CHANNEL 13 CHAN13: OUTPUT CHANNEL. # CHANNEL 13 CHAN13; OUTPUT CHANNEL.
# #
# BIT 1 RADAR C PROPER SETTING OF THE A,B,C MATRIX # BIT 1 RADAR C PROPER SETTING OF THE A,B,C MATRIX
# BIT 2 RADAR B SELECTS CERTAIN RADAR # BIT 2 RADAR B SELECTS CERTAIN RADAR
@ -99,7 +99,7 @@
# BIT 6 BLOCK INPUTS TO UPLINK CELL # BIT 6 BLOCK INPUTS TO UPLINK CELL
# BIT 7 DOWNLINK TELEMETRY WORD ORDER CODE BIT # BIT 7 DOWNLINK TELEMETRY WORD ORDER CODE BIT
# BIT 8 RHC COUNTER ENABLE (READ HAND CONTROLLER ANGLES) # BIT 8 RHC COUNTER ENABLE (READ HAND CONTROLLER ANGLES)
# BIT 9 START RHC READ INTO COUNTERS IS BIT 8 SET # BIT 9 START RHC READ INTO COUNTERS IF BIT 8 SET
# BIT 10 TEST ALARMS, TEST DSKY LIGHTS # BIT 10 TEST ALARMS, TEST DSKY LIGHTS
# BIT 11 ENABLE STANDBY # BIT 11 ENABLE STANDBY
# BIT 12 RESET TRAP 31-A ALWAYS APPEAR TO BE SET TO 0 # BIT 12 RESET TRAP 31-A ALWAYS APPEAR TO BE SET TO 0
@ -107,17 +107,17 @@
# BIT 14 RESET TRAP 32 ALWAYS APPEAR TO BE SET TO 0 # BIT 14 RESET TRAP 32 ALWAYS APPEAR TO BE SET TO 0
# BIT 15 ENABLE T6 RUPT # BIT 15 ENABLE T6 RUPT
# CHANNEL 14 CHAN14: OUTPUT CHANNEL; USED TO CONTROL COMPUTER COUNTER CELLS (CDU, GYRO, SPACECRAFT FUNC). # CHANNEL 14 CHAN14; OUTPUT CHANNEL; USED TO CONTROL COMPUTER COUNTER CELLS (CDU,GYRO,SPACECRAFT FUNC.
# #
# BIT 1 OUTLINK ACTIVITY (NOT USED) # BIT 1 OUTLINK ACTIVITY (NOT USED)
# BIT 2 ALTITUDE RATE OR ALTITUDE SELECTOR # BIT 2 ALTITUDE RATE OR ALTITIDE SELECTOR
# BIT 3 ALTITUDE METER ACTIVITY # BIT 3 ALTITUDE METER ACTIVITY
# BIT 4 THRUST DRIVE ACTIVITY FOR DESCENT ENGINE # BIT 4 THRUST DRIVE ACTIVITY FOR DESCENT ENGINE
# BIT 5 SPARE # BIT 5 SPARE
# BIT 6 GYRO ENABLE POWER FOR PULSES # BIT 6 GYRO ENABLE POWER FOR PULSES
# BIT 7 GYRO SELECT B PAIR OF BITS IDENTIFIES AXIS OF # BIT 7 GYRO SELECT B PAIR OF BITS IDENTIFIES AXIS OF -
# BIT 8 GYRO SELECT A GYRO SYSTEM TO BE TORQUED. # BIT 8 GYRO SELECT A GYRO SYSTEM TO BE TORQUED.
# BIT 9 GYRO TORQUING COMMAND IN NEGATIVE DIRECTION. # BIT 9 GYRO TORQUING COMMAND IN NEGATIVE DIRECTION
# Page 57 # Page 57
# BIT 10 GYRO ACTIVITY # BIT 10 GYRO ACTIVITY
# BIT 11 DRIVE CDU S # BIT 11 DRIVE CDU S
@ -126,11 +126,11 @@
# BIT 14 DRIVE CDU Y # BIT 14 DRIVE CDU Y
# BIT 15 DRIVE CDU X # BIT 15 DRIVE CDU X
# CHANNEL 15 MNKEYIN: INPUT CHANNEL; KEY CODE INPUT FROM KEYBOARD OF DSKY, SENSED BY PROGRAM WHEN # CHANNEL 15 MNKEYIN; INPUT CHANNEL;KEY CODE INPUT FROM KEYBOARD OF DSKY, SENSED BY PROGRAM WHEN
# PROGRAM INTERRUPT #5 IS RECEIVED. USED BITS 5-1 # PROGRAM INTERRUPT #5 IS RECEIVED. USES BITS 5-1
# CHANNEL 16 NAVKEYIN: INPUT CHANNEL; OPTICS MARK INFORMATION AND NAVIGATION PANEL DSKY (CM) OR THRUST # CHANNEL 16 NAVKEYIN; INPUT CHANNEL; OPTICS MARK INFORMATION AND NAVIGA ION PANEL DSKY (CM) OR THRUST
# CONTROL (LM) SENSED BY PROGRAM THEN PROGRAM INTERRUPT #6 IS RECEIVED. USES BITS 3-7 ONLY. # CONTROL (LM) SENSED BY PROGRAM WHEN PROGRAM INTER-RUPT #6 IS RECEIVED. USES BITS 3-7 ONLY.
# #
# BIT 1 NOT ASSIGNED # BIT 1 NOT ASSIGNED
# BIT 2 NOT ASSIGNED # BIT 2 NOT ASSIGNED
@ -155,7 +155,7 @@
# BIT 7 RR CDU FAIL # BIT 7 RR CDU FAIL
# BIT 8 SPARE # BIT 8 SPARE
# BIT 9 IMU OPERATE WITH NO MALFUNCTION # BIT 9 IMU OPERATE WITH NO MALFUNCTION
# BIT 10 LM COMPUTER (NOT AGS) HAS CONTROL OF LM. # BIT 10 LM COMPUTER (NOT AGS) HAS CONTROL OF LM
# BIT 11 IMU CAGE COMMAND TO DRIVE IMU GIMBAL ANGLES TO 0. # BIT 11 IMU CAGE COMMAND TO DRIVE IMU GIMBAL ANGLES TO 0.
# BIT 12 IMU CDU FAIL (MALFUNCTION OF IMU CDU,S) # BIT 12 IMU CDU FAIL (MALFUNCTION OF IMU CDU,S)
# BIT 13 IMU FAIL (MALFUNCTION OF IMU STABILIZATION LOOPS) # BIT 13 IMU FAIL (MALFUNCTION OF IMU STABILIZATION LOOPS)
@ -163,15 +163,15 @@
# BIT 15 TEMPERATURE OF STABLE MEMBER WITHIN DESIGN LIMITS # BIT 15 TEMPERATURE OF STABLE MEMBER WITHIN DESIGN LIMITS
# CHANNEL 31 INPUT CHANNEL; BITS ASSOCIATED WITH THE ATTITUDE CONTROLLER, TRANSLATIONAL CONTROLLER, # CHANNEL 31 INPUT CHANNEL; BITS ASSOCIATED WITH THE ATTITUDE CONTROLLER, TRANSLATIONAL CONTROLLER,
# AND SPACECRAFT ATTITUDE CONTROL; USED BY RCS DAP. # AND SPACECRAFT ATTITUDE CONTROL; USED BY RCS DAP
# #
# BIT 1 ROTATION (BY RHC) COMMANDED IN POSITIVE PITCH DIRECTION; MUST BE IN MINIMUM IMPULSE MODE. # BIT 1 ROTATION (BY RHC) COMMANDED IN POSITIVE PITCH DIRECTION; MUST BE IN MINIMUM IMPULSE MODE.
# ALSO POSITIVE ELEVATION CHANGE FOR LANDING POINT DESIGNATOR # ALSO POSITIVE ELEVATION CHANGE FOR LANDING POINT DESIGNATOR
# BIT 2 AS BIT 1 EXCEPT NEGATIVE PITCH AND ELEVATION. # BIT 2 AS BIT 1 EXCEPT NEGATIVE PITCH AND ELEVATION
# BIT 3 ROTATION (BY RHC) COMMANDED IN POSITIVE YAW DIRECTION; MUST BE IN MINIMUM IMPULSE MODE. # BIT 3 ROTATION (BY RHC) COMMANDED IN POSITIVE YAW DIRECTION; MUST BE IN MINIMUM IMPULSE MODE.
# BIT 4 AS BIT 3 EXCEPT NEGATIVE YAW # BIT 4 AS BIT 3 EXCEPT NEGATIVE YAW
# BIT 5 ROTATION (BY RHC) COMMANDED IN POSITIVE ROLL DIRECTION; MUST BE IN MINIMUM IMPULSE MODE. # BIT 5 ROTATION (BY RHC) COMMANDED IN POSITIVE ROLL DIRECTION; MUST BE IN MINIMUM IMPULSE MODE.
# ALSO POSITIVE AZIMUTH CHANGE FOR LANDING POINT DESIGNATOR. # ALSO POSITIVE AZIMUTH CHANGE FOR LANDING POINT DESIGNATOR
# BIT 6 AS BIT 5 EXCEPT NEGATIVE ROLL AND AZIMUTH # BIT 6 AS BIT 5 EXCEPT NEGATIVE ROLL AND AZIMUTH
# BIT 7 TRANSLATION IN +X DIRECTION COMMANDED BY THC # BIT 7 TRANSLATION IN +X DIRECTION COMMANDED BY THC
# BIT 8 TRANSLATION IN -X DIRECTION COMMANDED BY THC # BIT 8 TRANSLATION IN -X DIRECTION COMMANDED BY THC
@ -182,7 +182,7 @@
# Page 59 # Page 59
# BIT 13 ATTITUDE HOLD MODE ON SCS MODE CONTROL SWITCH # BIT 13 ATTITUDE HOLD MODE ON SCS MODE CONTROL SWITCH
# BIT 14 AUTO STABILIZATION OF ATTITUDE ON SCS MODE SWITCH # BIT 14 AUTO STABILIZATION OF ATTITUDE ON SCS MODE SWITCH
# BIT 15 ATTITUDE CONTROL OUT OF DETENT (RHC NOT IN NEUTRAL) # BIT 15 ATTITUDE CONTROL OUT OF DETENT (RHC NOT IN NEUTRAL
# CHANNEL 32 INPUT CHANNEL. # CHANNEL 32 INPUT CHANNEL.
# #
@ -194,11 +194,11 @@
# BIT 6 THRUSTERS 13 & 15 DISABLED BY CREW # BIT 6 THRUSTERS 13 & 15 DISABLED BY CREW
# BIT 7 THRUSTERS 9 & 12 DISABLED BY CREW # BIT 7 THRUSTERS 9 & 12 DISABLED BY CREW
# BIT 8 THRUSTERS 10 & 11 DISABLED BY CREW # BIT 8 THRUSTERS 10 & 11 DISABLED BY CREW
# BIT 9 DESCENT ENGINE DISABLED BY CREW # BIT 9 DESCENT ENGINE GIMBALS DISABLED BY CREW
# BIT 10 APPARENT DESCENT ENGINE GIMBAL FAILURE # BIT 10 APPARENT DESCENT ENGINE GIMBAL FAILURE
# BIT 14 INDICATES PROCEED KEY IS DEPRESSED # BIT 14 INDICATES PROCEED KEY IS DEPRESSED
# CHANNEL 33 CHAN33: INPUT CHANNEL; FOR HARDWARE STATUS AND COMMAND INFORMATION. BITS 15-11 ARE FLIP- # CHANNEL 33 CHAN33; INPUT CHANNEL; FOR HARDWARE STATUS AND COMMAND INFORMATION. BITS 15-11 ARE FLIP-
# FLOP BITS RESET BY A CHANNEL "WRITE" COMMAND THAT ARE RESET BY A RESTART & BY T4RUPT LOOP. # FLOP BITS RESET BY A CHANNEL "WRITE" COMMAND THAT ARE RESET BY A RESTART & BY T4RUPT LOOP.
# #
# BIT 1 SPARE # BIT 1 SPARE
@ -215,10 +215,9 @@
# BIT 11 UPLINK TOO FAST # BIT 11 UPLINK TOO FAST
# BIT 12 DOWNLINK TOO FAST # BIT 12 DOWNLINK TOO FAST
# BIT 13 PIPA FAIL # BIT 13 PIPA FAIL
# BIT 14 WARNING OF REPEATED ALARMS: RESTART, COUNTER FAIL, VOLTAGE FAIL, AND SCALAR DOUBLE. # BIT 14 WARNING OF REPEATED ALARMS: RESTART,COUNTER FAIL, VOLTAGE FAIL,AND SCALAR DOUBLE.
# BIT 15 LGC OSCILLATOR STOPPED # BIT 15 LGC OSCILLATOR STOPPED
# CHANNEL 34 DNT M1: OUTPUT CHANNEL; DOWNLINK 1: FIRST OF TWO WORDS SERIALIZATION. # CHANNEL 34 DNT M1; OUTPUT CHANNEL; DOWNLINK 1 FIRST OF TWO WORDS SERIALIZATION.
# CHANNEL 35 DNT M2: OUTPUT CHANNEL; DOWNLINK 2: SECOND OF TWO WORDS SERIALIZATION. # CHANNEL 35 DNT M2; OUTPUT CHANNEL DOWNLINK 2 SOCOND OF TWO WORDS SERIALIZATION.