From 422050965990dfa8ad1ffe4ae92e793d7d1ddae5 Mon Sep 17 00:00:00 2001 From: panoreak Date: Sat, 10 Oct 2020 22:01:06 -0400 Subject: [PATCH] Proof INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.acg #592 (#708) Co-authored-by: James Harris --- .../INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.agc | 317 +++++++++--------- 1 file changed, 158 insertions(+), 159 deletions(-) diff --git a/Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.agc b/Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.agc index 60b76e8..3c48548 100644 --- a/Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.agc +++ b/Luminary099/INPUT_OUTPUT_CHANNEL_BIT_DESCRIPTIONS.agc @@ -26,199 +26,198 @@ # 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 -# FACTOR IS B23 IN CSEC, SO MAX VALUE ABOUT 23.3 HOURS AND LEAST SIGNIFICANT BIT 5.12 SECS. +# 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. -# 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 -# SIGNIFICANT BIT IS 1/3200 SEC. SCALE FACTOR OF D.P. WORD WITH CHANNEL 3 IS B23 CSEC. +# 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 +# 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 -# APPROPRIATE FIXED MEMORY BANK IF FBANK IS 30 OCTAL OR MORE. USES BITS 5-7. +# 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. -# 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 -# CHANGED AND BITS 11-1 CONTAIN THE REQUIRED SETTINGS FOR THE RELAYS IN THE ROW. +# 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 +# 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 -# DRIVE INDIVIDUAL INDICATORS OF THE DISPLAY SYSTEM. BITS 1-7 ARE A RELAYS. +# 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. # -# BIT 1 ISS WARNING -# BIT 2 LIGHT COMPUTER ACTIVITY LAMP -# BIT 3 LIGHT UPLINK ACTIVITY LAMP -# BIT 4 LIGHT TEMP CAUTION LAMP -# BIT 5 LIGHT KEYBOARD RELEASE LAMP -# BIT 6 FLASH VERB AND NOUN LAMPS -# BIT 7 LIGHT OPERATOR ERROR LAMP +# BIT 1 ISS WARNING +# BIT 2 LIGHT COMPUTER ACTIVITY LAMP +# BIT 3 LIGHT UPLINK ACTIVITY LAMP +# BIT 4 LIGHT TEMP CAUTION LAMP +# BIT 5 LIGHT KEYBOARD RELEASE LAMP +# BIT 6 FLASH VERB AND NOUN LAMPS +# BIT 7 LIGHT OPERATOR ERROR LAMP # Page 55 -# BIT 8 SPARE -# BIT 9 TEST CONNECTOR OUTBIT -# BIT 10 CAUTION RESET -# BIT 11 SPARE -# BIT 12 SPARE -# BIT 13 ENGINE ON -# BIT 14 ENGINE OFF -# BIT 15 SPARE +# BIT 8 SPARE +# BIT 9 TEST CONNECTOR OUTBIT +# BIT 10 CAUTION RESET +# BIT 11 SPARE +# BIT 12 SPARE +# BIT 13 ENGINE ON +# BIT 14 ENGINE OFF +# 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 2 ENABLE CDU RADAR ERROR COUNTERS -# BIT 3 NOT USED -# BIT 4 COARSE ALIGN ENABLE OF IMU -# BIT 5 ZERO IMU CDU'S -# BIT 6 ENABLE IMU ERROR COUNTER, CDU ERROR COUNTER. -# BIT 7 SPARE -# BIT 8 DISPLAY INERTIAL DATA -# BIT 9 -PITCH GIMBAL TRIM (BELL MOTION) DESCENT ENGINE -# BIT 10 +PITCH 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 13 LR POSITION 2 COMMAND -# BIT 14 ENABLE RENDEZVOUS RADAR LOCK-ON; AUTO ANGLE TRACK'G -# BIT 15 ISS TURN ON DELAY COMPLETE +# BIT 1 ZERO RR CDU; CDU'S GIVE RRADAR INFORMATION FOR LM +# BIT 2 ENABLE CDU RADAR ERROR COUNTERS +# BIT 3 NOT USED +# BIT 4 COARSE ALIGN ENABLE OF IMU +# BIT 5 ZERO IMU CDU'S +# BIT 6 ENABLE IMU ERROR COUNTER, CDU ERROR COUNTER. +# BIT 7 SPARE +# BIT 8 DISPLAY INERTIAL DATA +# BIT 9 -PITCH GIMBAL TRIM (BELL MOTION) DESCENT ENGINE +# BIT 10 +PITCH 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 13 LR POSITION 2 COMMAND +# BIT 14 ENABLE RENDESVOUS RADAR LOCK-ON;AUTO ANGLE TRACK'G +# BIT 15 ISS TURN ON DELAY COMPLETE # 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 2 RADAR B SELECTS CERTAIN RADAR -# BIT 3 RADAR A PARAMETERS TO BE READ. -# BIT 4 RADAR ACTIVITY -# BIT 5 NOT USED (CONNECTS AN ALTERNATE INPUT TO UPLINK) -# BIT 6 BLOCK INPUTS TO UPLINK CELL -# BIT 7 DOWNLINK TELEMETRY WORD ORDER CODE BIT -# BIT 8 RHC COUNTER ENABLE (READ HAND CONTROLLER ANGLES) -# BIT 9 START RHC READ INTO COUNTERS IS BIT 8 SET -# BIT 10 TEST ALARMS, TEST DSKY LIGHTS -# BIT 11 ENABLE STANDBY -# BIT 12 RESET TRAP 31-A ALWAYS APPEAR TO BE SET TO 0 -# BIT 13 RESET TRAP 31-B 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 1 RADAR C PROPER SETTING OF THE A,B,C MATRIX +# BIT 2 RADAR B SELECTS CERTAIN RADAR +# BIT 3 RADAR A PARAMETERS TO BE READ. +# BIT 4 RADAR ACTIVITY +# BIT 5 NOT USED (CONNECTS AN ALTERNATE INPUT TO UPLINK) +# BIT 6 BLOCK INPUTS TO UPLINK CELL +# BIT 7 DOWNLINK TELEMETRY WORD ORDER CODE BIT +# BIT 8 RHC COUNTER ENABLE (READ HAND CONTROLLER ANGLES) +# BIT 9 START RHC READ INTO COUNTERS IF BIT 8 SET +# BIT 10 TEST ALARMS, TEST DSKY LIGHTS +# BIT 11 ENABLE STANDBY +# BIT 12 RESET TRAP 31-A ALWAYS APPEAR TO BE SET TO 0 +# BIT 13 RESET TRAP 31-B ALWAYS APPEAR TO BE SET TO 0 +# BIT 14 RESET TRAP 32 ALWAYS APPEAR TO BE SET TO 0 +# 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 2 ALTITUDE RATE OR ALTITUDE SELECTOR -# BIT 3 ALTITUDE METER ACTIVITY -# BIT 4 THRUST DRIVE ACTIVITY FOR DESCENT ENGINE -# BIT 5 SPARE -# BIT 6 GYRO ENABLE POWER FOR PULSES -# BIT 7 GYRO SELECT B PAIR OF BITS IDENTIFIES AXIS OF -# BIT 8 GYRO SELECT A GYRO SYSTEM TO BE TORQUED. -# BIT 9 GYRO TORQUING COMMAND IN NEGATIVE DIRECTION. +# BIT 1 OUTLINK ACTIVITY (NOT USED) +# BIT 2 ALTITUDE RATE OR ALTITIDE SELECTOR +# BIT 3 ALTITUDE METER ACTIVITY +# BIT 4 THRUST DRIVE ACTIVITY FOR DESCENT ENGINE +# BIT 5 SPARE +# BIT 6 GYRO ENABLE POWER FOR PULSES +# BIT 7 GYRO SELECT B PAIR OF BITS IDENTIFIES AXIS OF - +# BIT 8 GYRO SELECT A GYRO SYSTEM TO BE TORQUED. +# BIT 9 GYRO TORQUING COMMAND IN NEGATIVE DIRECTION # Page 57 -# BIT 10 GYRO ACTIVITY -# BIT 11 DRIVE CDU S -# BIT 12 DRIVE CDU T -# BIT 13 DRIVE CDU Z -# BIT 14 DRIVE CDU Y -# BIT 15 DRIVE CDU X +# BIT 10 GYRO ACTIVITY +# BIT 11 DRIVE CDU S +# BIT 12 DRIVE CDU T +# BIT 13 DRIVE CDU Z +# BIT 14 DRIVE CDU Y +# BIT 15 DRIVE CDU X -# 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 +# CHANNEL 15 MNKEYIN; INPUT CHANNEL;KEY CODE INPUT FROM KEYBOARD OF DSKY, SENSED BY PROGRAM WHEN +# PROGRAM INTERRUPT #5 IS RECEIVED. USES BITS 5-1 -# CHANNEL 16 NAVKEYIN: INPUT CHANNEL; OPTICS MARK INFORMATION AND NAVIGATION PANEL DSKY (CM) OR THRUST -# CONTROL (LM) SENSED BY PROGRAM THEN PROGRAM INTERRUPT #6 IS RECEIVED. USES BITS 3-7 ONLY. +# CHANNEL 16 NAVKEYIN; INPUT CHANNEL; OPTICS MARK INFORMATION AND NAVIGA ION PANEL DSKY (CM) OR THRUST +# CONTROL (LM) SENSED BY PROGRAM WHEN PROGRAM INTER-RUPT #6 IS RECEIVED. USES BITS 3-7 ONLY. # -# BIT 1 NOT ASSIGNED -# BIT 2 NOT ASSIGNED -# BIT 3 OPTICS X-AXIS MARK SIGNAL FOR ALIGN OPTICAL TSCOPE -# BIT 4 OPTICS Y-AXIS MARK SIGNAL FOR AOT -# BIT 5 OPTICS MARK REJECT SIGNAL -# BIT 6 DESCENT+ ; CREW DESIRED SLOWING RATE OF DESCENT -# BIT 7 DESCENT- ; CREW DESIRED SPEEDING UP RATE OF D'CENT +# BIT 1 NOT ASSIGNED +# BIT 2 NOT ASSIGNED +# BIT 3 OPTICS X-AXIS MARK SIGNAL FOR ALIGN OPTICAL TSCOPE +# BIT 4 OPTICS Y-AXIS MARK SIGNAL FOR AOT +# BIT 5 OPTICS MARK REJECT SIGNAL +# BIT 6 DESCENT+ ; CREW DESIRED SLOWING RATE OF DESCENT +# BIT 7 DESCENT- ; CREW DESIRED SPEEDING UP RATE OF D'CENT -# NOTE: ALL BITS IN CHANNELS 30-33 ARE INVERTED AS SENSED BY THE PROGRAM, SO THAT A VALUE OF ZERO MEANS +# NOTE: ALL BITS IN CHANNELS 30-33 ARE INVERTED AS SENSED BY THE PROGRAM, SO THAT A VALUE OF ZERO MEANS # THAT THE INDICATED SIGNAL IS PRESENT. -# CHANNEL 30 INPUT CHANNEL +# CHANNEL 30 INPUT CHANNEL # -# BIT 1 ABORT WITH DESCENT STAGE -# BIT 2 UNUSED -# BIT 3 ENGINE ARMED SIGNAL -# BIT 4 ABORT WITH ASCENT ENGINE STAGE -# BIT 5 AUTO THROTTLE; COMPUTER CONTROL OF DESCENT ENGINE +# BIT 1 ABORT WITH DESCENT STAGE +# BIT 2 UNUSED +# BIT 3 ENGINE ARMED SIGNAL +# BIT 4 ABORT WITH ASCENT ENGINE STAGE +# BIT 5 AUTO THROTTLE; COMPUTER CONTROL OF DESCENT ENGINE # Page 58 -# BIT 6 DISPLAY INERTIAL DATA -# BIT 7 RR CDU FAIL -# BIT 8 SPARE -# BIT 9 IMU OPERATE WITH NO MALFUNCTION -# BIT 10 LM COMPUTER (NOT AGS) HAS CONTROL OF LM. -# BIT 11 IMU CAGE COMMAND TO DRIVE IMU GIMBAL ANGLES TO 0. -# BIT 12 IMU CDU FAIL (MALFUNCTION OF IMU CDU,S) -# BIT 13 IMU FAIL (MALFUNCTION OF IMU STABILIZATION LOOPS) -# BIT 14 ISS TURN ON REQUESTED -# BIT 15 TEMPERATURE OF STABLE MEMBER WITHIN DESIGN LIMITS +# BIT 6 DISPLAY INERTIAL DATA +# BIT 7 RR CDU FAIL +# BIT 8 SPARE +# BIT 9 IMU OPERATE WITH NO MALFUNCTION +# BIT 10 LM COMPUTER (NOT AGS) HAS CONTROL OF LM +# BIT 11 IMU CAGE COMMAND TO DRIVE IMU GIMBAL ANGLES TO 0. +# BIT 12 IMU CDU FAIL (MALFUNCTION OF IMU CDU,S) +# BIT 13 IMU FAIL (MALFUNCTION OF IMU STABILIZATION LOOPS) +# BIT 14 ISS TURN ON REQUESTED +# BIT 15 TEMPERATURE OF STABLE MEMBER WITHIN DESIGN LIMITS -# CHANNEL 31 INPUT CHANNEL; BITS ASSOCIATED WITH THE ATTITUDE CONTROLLER, TRANSLATIONAL CONTROLLER, -# AND SPACECRAFT ATTITUDE CONTROL; USED BY RCS DAP. +# CHANNEL 31 INPUT CHANNEL; BITS ASSOCIATED WITH THE ATTITUDE CONTROLLER, TRANSLATIONAL CONTROLLER, +# AND SPACECRAFT ATTITUDE CONTROL; USED BY RCS DAP # -# BIT 1 ROTATION (BY RHC) COMMANDED IN POSITIVE PITCH DIRECTION; MUST BE IN MINIMUM IMPULSE MODE. -# ALSO POSITIVE ELEVATION CHANGE FOR LANDING POINT DESIGNATOR -# 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 4 AS BIT 3 EXCEPT NEGATIVE YAW -# BIT 5 ROTATION (BY RHC) COMMANDED IN POSITIVE ROLL DIRECTION; MUST BE IN MINIMUM IMPULSE MODE. -# ALSO POSITIVE AZIMUTH CHANGE FOR LANDING POINT DESIGNATOR. -# BIT 6 AS BIT 5 EXCEPT NEGATIVE ROLL AND AZIMUTH -# BIT 7 TRANSLATION IN +X DIRECTION COMMANDED BY THC -# BIT 8 TRANSLATION IN -X DIRECTION COMMANDED BY THC -# BIT 9 TRANSLATION IN +Y DIRECTION COMMANDED BY THC -# BIT 10 TRANSLATION IN -Y DIRECTION COMMANDED BY THC -# BIT 11 TRANSLATION IN +Z DIRECTION COMMANDED BY THC -# BIT 12 TRANSLATION IN -Z DIRECTION COMMANDED BY THC +# BIT 1 ROTATION (BY RHC) COMMANDED IN POSITIVE PITCH DIRECTION; MUST BE IN MINIMUM IMPULSE MODE. +# ALSO POSITIVE ELEVATION CHANGE FOR LANDING POINT DESIGNATOR +# 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 4 AS BIT 3 EXCEPT NEGATIVE YAW +# BIT 5 ROTATION (BY RHC) COMMANDED IN POSITIVE ROLL DIRECTION; MUST BE IN MINIMUM IMPULSE MODE. +# ALSO POSITIVE AZIMUTH CHANGE FOR LANDING POINT DESIGNATOR +# BIT 6 AS BIT 5 EXCEPT NEGATIVE ROLL AND AZIMUTH +# BIT 7 TRANSLATION IN +X DIRECTION COMMANDED BY THC +# BIT 8 TRANSLATION IN -X DIRECTION COMMANDED BY THC +# BIT 9 TRANSLATION IN +Y DIRECTION COMMANDED BY THC +# BIT 10 TRANSLATION IN -Y DIRECTION COMMANDED BY THC +# BIT 11 TRANSLATION IN +Z DIRECTION COMMANDED BY THC +# BIT 12 TRANSLATION IN -Z DIRECTION COMMANDED BY THC # Page 59 -# BIT 13 ATTITUDE HOLD MODE ON SCS MODE CONTROL SWITCH -# BIT 14 AUTO STABILIZATION OF ATTITUDE ON SCS MODE SWITCH -# BIT 15 ATTITUDE CONTROL OUT OF DETENT (RHC NOT IN NEUTRAL) +# BIT 13 ATTITUDE HOLD MODE ON SCS MODE CONTROL SWITCH +# BIT 14 AUTO STABILIZATION OF ATTITUDE ON SCS MODE SWITCH +# BIT 15 ATTITUDE CONTROL OUT OF DETENT (RHC NOT IN NEUTRAL -# CHANNEL 32 INPUT CHANNEL. +# CHANNEL 32 INPUT CHANNEL. # -# BIT 1 THRUSTERS 2 & 4 DISABLED BY CREW -# BIT 2 THRUSTERS 5 & 8 DISABLED BY CREW -# BIT 3 THRUSTERS 1 & 3 DISABLED BY CREW -# BIT 4 THRUSTERS 6 & 7 DISABLED BY CREW -# BIT 5 THRUSTERS 14 & 16 DISABLED BY CREW -# BIT 6 THRUSTERS 13 & 15 DISABLED BY CREW -# BIT 7 THRUSTERS 9 & 12 DISABLED BY CREW -# BIT 8 THRUSTERS 10 & 11 DISABLED BY CREW -# BIT 9 DESCENT ENGINE DISABLED BY CREW -# BIT 10 APPARENT DESCENT ENGINE GIMBAL FAILURE -# BIT 14 INDICATES PROCEED KEY IS DEPRESSED +# BIT 1 THRUSTERS 2 & 4 DISABLED BY CREW +# BIT 2 THRUSTERS 5 & 8 DISABLED BY CREW +# BIT 3 THRUSTERS 1 & 3 DISABLED BY CREW +# BIT 4 THRUSTERS 6 & 7 DISABLED BY CREW +# BIT 5 THRUSTERS 14 & 16 DISABLED BY CREW +# BIT 6 THRUSTERS 13 & 15 DISABLED BY CREW +# BIT 7 THRUSTERS 9 & 12 DISABLED BY CREW +# BIT 8 THRUSTERS 10 & 11 DISABLED BY CREW +# BIT 9 DESCENT ENGINE GIMBALS DISABLED BY CREW +# BIT 10 APPARENT DESCENT ENGINE GIMBAL FAILURE +# BIT 14 INDICATES PROCEED KEY IS DEPRESSED -# 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. +# 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. # -# BIT 1 SPARE -# BIT 2 RR AUTO-POWER ON -# BIT 3 RR RANGE LOW SCALE -# BIT 4 RR DATA GOOD -# BIT 5 LR RANGE DATA GOOD -# BIT 6 LR POS1 -# BIT 7 LR POS2 +# BIT 1 SPARE +# BIT 2 RR AUTO-POWER ON +# BIT 3 RR RANGE LOW SCALE +# BIT 4 RR DATA GOOD +# BIT 5 LR RANGE DATA GOOD +# BIT 6 LR POS1 +# BIT 7 LR POS2 # Page 60 -# BIT 8 LR VEL DATA GOOD -# BIT 9 LR RANGE LOW SCALE -# BIT 10 BLOCK UPLINK INPUT -# BIT 11 UPLINK TOO FAST -# BIT 12 DOWNLINK TOO FAST -# BIT 13 PIPA FAIL -# BIT 14 WARNING OF REPEATED ALARMS: RESTART, COUNTER FAIL, VOLTAGE FAIL, AND SCALAR DOUBLE. -# BIT 15 LGC OSCILLATOR STOPPED - -# 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. +# BIT 8 LR VEL DATA GOOD +# BIT 9 LR RANGE LOW SCALE +# BIT 10 BLOCK UPLINK INPUT +# BIT 11 UPLINK TOO FAST +# BIT 12 DOWNLINK TOO FAST +# BIT 13 PIPA FAIL +# BIT 14 WARNING OF REPEATED ALARMS: RESTART,COUNTER FAIL, VOLTAGE FAIL,AND SCALAR DOUBLE. +# BIT 15 LGC OSCILLATOR STOPPED +# CHANNEL 34 DNT M1; OUTPUT CHANNEL; DOWNLINK 1 FIRST OF TWO WORDS SERIALIZATION. +# CHANNEL 35 DNT M2; OUTPUT CHANNEL DOWNLINK 2 SOCOND OF TWO WORDS SERIALIZATION.