2016-07-31 22:32:55 +00:00
|
|
|
# Copyright: Public domain.
|
|
|
|
|
# Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
|
|
|
|
|
# Purpose: Part of the source code for Luminary 1A build 099.
|
|
|
|
|
# It is part of the source code for the Lunar Module's (LM)
|
|
|
|
|
# Apollo Guidance Computer (AGC), for Apollo 11.
|
|
|
|
|
#
|
|
|
|
|
# Assembler: yaYUL
|
|
|
|
|
# Contact: Jim Lawton <jim.lawton@gmail.com>
|
|
|
|
|
# Website: www.ibiblio.org/apollo.
|
|
|
|
|
# Pages: 001-027
|
|
|
|
|
# Mod history: 2009-05-16 JVL Transcribed from page images.
|
|
|
|
|
#
|
|
|
|
|
# This source code has been transcribed or otherwise adapted from digitized
|
|
|
|
|
# images of a hardcopy from the MIT Museum. The digitization was performed
|
|
|
|
|
# by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
|
|
|
|
|
# thanks to both. The images (with suitable reduction in storage size and
|
|
|
|
|
# consequent reduction in image quality as well) are available online at
|
|
|
|
|
# www.ibiblio.org/apollo. If for some reason you find that the images are
|
|
|
|
|
# illegible, contact me at info@sandroid.org about getting access to the
|
|
|
|
|
# (much) higher-quality images which Paul actually created.
|
|
|
|
|
#
|
|
|
|
|
# Notations on the hardcopy document read, in part:
|
|
|
|
|
#
|
|
|
|
|
# Assemble revision 001 of AGC program LMY99 by NASA 2021112-061
|
|
|
|
|
# 16:27 JULY 14, 1969
|
|
|
|
|
|
|
|
|
|
# Page 1
|
|
|
|
|
|
|
|
|
|
# THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
|
|
|
|
|
# THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
|
|
|
|
|
|
|
|
|
|
# GUIDANCE SYSTEM OPERATIONS PLAN
|
|
|
|
|
# FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
|
|
|
|
|
# USING PROGRAM LUMINARY
|
|
|
|
|
|
2016-12-28 16:11:25 +00:00
|
|
|
# THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
|
2016-07-31 22:32:55 +00:00
|
|
|
# TECHNOLOGY, 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS, UNDER PROJECT 55-238-70, SPONSORED BY THE MANNED
|
|
|
|
|
# SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
|
|
|
|
|
|
|
|
|
|
# THIS PROGRAM IS REFERRED TO AS LUMINARY 1A
|
|
|
|
|
|
|
|
|
|
# Page 2
|
|
|
|
|
|
|
|
|
|
# TABLE OF LOG CARDS
|
|
|
|
|
# ASSEMBLY AND OPERATION INFORMATION
|
|
|
|
|
# TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
|
|
|
|
|
# CONTROLLED CONSTANTS
|
|
|
|
|
# INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
|
|
|
|
|
# FLAGWORD ASSIGNMENTS
|
|
|
|
|
# SUBROUTINE CALLS
|
|
|
|
|
|
|
|
|
|
# TABLE OF SUBROUTINE LOG SECTIONS
|
|
|
|
|
# LUMERASE
|
|
|
|
|
# ERASABLE ASSIGNMENTS
|
|
|
|
|
# LNYAIDE
|
|
|
|
|
# INTERRUPT LEAD INS
|
|
|
|
|
# T4RUPT PROGRAM
|
|
|
|
|
# RCS FAILURE MONITOR
|
|
|
|
|
# DOWNLINK LISTS
|
|
|
|
|
# AGS INITIALIZATION
|
|
|
|
|
# FRESH START AND RESTART
|
|
|
|
|
# RESTART TABLES
|
|
|
|
|
# AOTMARK
|
|
|
|
|
# EXTENDED VERBS
|
|
|
|
|
# PINBALL NOUN TABLES
|
|
|
|
|
# LEM GEOMETRY
|
|
|
|
|
# IMU COMPENSATION PACKAGE
|
|
|
|
|
# R63
|
|
|
|
|
# ATTITUDE MANEUVER ROUTINE
|
|
|
|
|
# GIMBAL LOCK AVOIDANCE
|
|
|
|
|
# KALCMANU STEERING
|
|
|
|
|
# SYSTEM TEST STANDARD LEAD INS
|
|
|
|
|
# IMU PERFORMANCE TESTS 2
|
|
|
|
|
# IMU PERFORMANCE TESTS 4
|
|
|
|
|
# PINBALL GAMES BUTTONS AND LIGHTS
|
|
|
|
|
# R60,R62
|
|
|
|
|
# S-BAND ANTENNA FOR LM
|
|
|
|
|
# LEMP20S
|
|
|
|
|
# RADAR LEADIN ROUTINES
|
|
|
|
|
# P20-P25
|
|
|
|
|
# LEMP30S
|
|
|
|
|
# P30,P37
|
|
|
|
|
# P32-P35, P72-P75
|
|
|
|
|
# GENERAL LAMBERT AIMPOINT GUIDANCE
|
|
|
|
|
# KISSING
|
|
|
|
|
# GROUND TRACKING DETERMINATION PROGRAM - P21
|
|
|
|
|
# P34-P35, P74-P75
|
|
|
|
|
# R31
|
|
|
|
|
# P76
|
|
|
|
|
# R30
|
|
|
|
|
# STABLE ORBIT - P38-P39
|
|
|
|
|
# Page 3
|
|
|
|
|
# FLY
|
|
|
|
|
# BURN, BABY, BURN -- MASTER IGNITION ROUTINE
|
|
|
|
|
# P40-P47
|
|
|
|
|
# THE LUNAR LANDING
|
|
|
|
|
# THROTTLE CONTROL ROUTINES
|
|
|
|
|
# LUNAR LANDING GUIDANCE EQUATIONS
|
|
|
|
|
# P70-P71
|
|
|
|
|
# P12
|
|
|
|
|
# ASCENT GUIDANCE
|
|
|
|
|
# SERVICER
|
|
|
|
|
# LANDING ANALOG DISPLAYS
|
|
|
|
|
# FINDCDUW -- GUIDAP INTERFACE
|
|
|
|
|
# LEMP50S
|
|
|
|
|
# P51-P53
|
|
|
|
|
# LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
|
|
|
|
|
# SKIPPER
|
|
|
|
|
# DOWN-TELEMETRY PROGRAM
|
|
|
|
|
# INTER-BANK COMMUNICATION
|
|
|
|
|
# INTEPRETER
|
|
|
|
|
# FIXED-FIXED CONSTANT POOL
|
|
|
|
|
# INTERPRETIVE CONSTANTS
|
|
|
|
|
# SINGLE PRECISION SUBROUTINES
|
|
|
|
|
# EXECUTIVE
|
|
|
|
|
# WAITLIST
|
|
|
|
|
# LATITUDE LONGITUDE SUBROUTINES
|
|
|
|
|
# PLANETARY INERTIAL ORIENTATION
|
|
|
|
|
# MEASUREMENT INCORPORATION
|
|
|
|
|
# CONIC SUBROUTINES
|
|
|
|
|
# INTEGRATION INITIALIZATION
|
|
|
|
|
# ORBITAL INTEGRATION
|
|
|
|
|
# INFLIGHT ALIGNMENT ROUTINES
|
|
|
|
|
# POWERED FLIGHT SUBROUTINES
|
|
|
|
|
# TIME OF FREE FALL
|
|
|
|
|
# AGC BLOCK TWO SELF-CHECK
|
|
|
|
|
# PHASE TABLE MAINTENANCE
|
|
|
|
|
# RESTARTS ROUTINE
|
|
|
|
|
# IMU MODE SWITCHING ROUTINES
|
|
|
|
|
# KEYRUPT, UPRUPT
|
|
|
|
|
# DISPLAY INTERFACE ROUTINES
|
|
|
|
|
# SERVICE ROUTINES
|
|
|
|
|
# ALARM AND ABORT
|
|
|
|
|
# UPDATE PROGRAM
|
|
|
|
|
# RTB OP CODES
|
|
|
|
|
# LMDAP
|
|
|
|
|
# T6-RUPT PROGRAMS
|
|
|
|
|
# DAP INTERFACE SUBROUTINES
|
|
|
|
|
# DAPIDLER PROGRAM
|
|
|
|
|
# P-AXIS RCS AUTOPILOT
|
|
|
|
|
# Q,R-AXIS RCS AUTOPILOT
|
|
|
|
|
# TJET LAW
|
|
|
|
|
# Page 4
|
|
|
|
|
# KALMAN FILTER
|
|
|
|
|
# TRIM GIMBAL CONTROL SYSTEM
|
|
|
|
|
# AOSTASK AND AOSJOB
|
|
|
|
|
# SPS BACK-UP RCS CONTROL
|
|
|
|
|
#
|
|
|
|
|
# SYMBOL TABLE LISTING
|
|
|
|
|
# UNREFERENCED SYMBOL LISTING
|
|
|
|
|
# ERASABLE & EQUALS CROSS-REFERENCE TABLE
|
|
|
|
|
# SUMMARY OF SYMBOL TABLE LISTINGS
|
|
|
|
|
# MEMORY TYPE & AVAILABILITY DISPLAY
|
|
|
|
|
# COUNT TABLE
|
|
|
|
|
# PARAGRAPHS GENERATED FOR THIS ASSEMBLY
|
|
|
|
|
# OCTAL LISTING
|
|
|
|
|
# OCCUPIED LOCATIONS TABLE
|
|
|
|
|
# SUBROS CALLED & PROGRAM STATUS
|
|
|
|
|
|
|
|
|
|
# Page 5
|
|
|
|
|
# VERB LIST FOR LUMINARY
|
|
|
|
|
|
|
|
|
|
# REGULAR VERBS
|
|
|
|
|
|
|
|
|
|
# 00 NOT IN USE
|
|
|
|
|
# 01 DISPLAY OCTAL COMP 1 IN R1
|
|
|
|
|
# 02 DISPLAY OCTAL COMP 2 IN R1
|
|
|
|
|
# 03 DISPLAY OCTAL COMP 3 IN R1
|
|
|
|
|
# 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
|
|
|
|
|
# 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
|
|
|
|
|
# 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
|
|
|
|
|
# 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
|
|
|
|
|
# 08
|
|
|
|
|
# 09
|
|
|
|
|
# 10
|
|
|
|
|
# 11 MONITOR OCTAL COMP 1 IN R1
|
|
|
|
|
# 12 MONITOR OCTAL COMP 2 IN R1
|
|
|
|
|
# 13 MONITOR OCTAL COMP 3 IN R1
|
|
|
|
|
# 14 MONITOR OCTAL COMP 1,2 IN R1,R2
|
|
|
|
|
# 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
|
|
|
|
|
# 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
|
2016-12-28 16:11:25 +00:00
|
|
|
# 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
|
2016-07-31 22:32:55 +00:00
|
|
|
# 18
|
|
|
|
|
# 19
|
|
|
|
|
# 20
|
|
|
|
|
# 21 LOAD COMPONENT 1 INTO R1
|
|
|
|
|
# 22 LOAD COMPONENT 2 INTO R2
|
|
|
|
|
# 23 LOAD COMPONENT 3 INTO R3
|
|
|
|
|
# 24 LOAD COMPONENT 1,2, INTO R1,R2
|
|
|
|
|
# 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
|
|
|
|
|
# 26
|
|
|
|
|
# 27 DISPLAY FIXED MEMORY
|
|
|
|
|
# 28
|
|
|
|
|
# 29
|
|
|
|
|
# 30 REQUEST EXECUTIVE
|
|
|
|
|
# 31 REQUEST WAITLIST
|
|
|
|
|
# 32 RECYCLE PROGRAM
|
|
|
|
|
# 33 PROCEED WITHOUT DSKY INPUTS
|
|
|
|
|
# 34 TERMINATE FUNCTION
|
|
|
|
|
# 35 TEST LIGHTS
|
|
|
|
|
# 36 REQUEST FRESH START
|
|
|
|
|
# 37 CHANGE PROGRAM (MAJOR MODE)
|
|
|
|
|
# 38
|
|
|
|
|
# 39
|
|
|
|
|
|
|
|
|
|
# Page 6
|
|
|
|
|
# EXTENDED VERBS
|
|
|
|
|
|
|
|
|
|
# 40 XERO CDU-S
|
|
|
|
|
# 41 COARSE ALIGN CDU-S
|
|
|
|
|
# 42 FINE ALIGN IMU
|
|
|
|
|
# 43 LOAD IMU ATT ERROR METERS
|
|
|
|
|
# 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
|
|
|
|
|
# 45
|
|
|
|
|
# 46
|
|
|
|
|
# 47 INITIALIZE AGS (R47)
|
|
|
|
|
# 48 REQUEST DAP DATA LOAD ROUTINE (R03)
|
|
|
|
|
# 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
|
|
|
|
|
# 50 PLEASE PERFORM
|
|
|
|
|
# 51
|
|
|
|
|
# 52 MARK X-RETICLE
|
|
|
|
|
# 53 MARK Y-RETICLE
|
|
|
|
|
# 54 MARK X OR Y-RETICLE
|
|
|
|
|
# 55 INCREMENT AGC TIME (DECIMAL)
|
|
|
|
|
# 56 TERMINATE TRACKING (P20 + P25)
|
|
|
|
|
# 57 PERMIT LANDING RADAR UPDATES
|
|
|
|
|
# 58 INHIBIT LANDING RADAR UPDATES
|
|
|
|
|
# 59
|
|
|
|
|
# 60 COMMAND LR TO POSITON 2.
|
|
|
|
|
# 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
|
|
|
|
|
# 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
|
|
|
|
|
# 63 SAMPLE RADAR ONCE PER SECOND (R04).
|
|
|
|
|
# 64 REQUEST S-BAND ANTENNA ROUTINE (R05).
|
|
|
|
|
# 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
|
|
|
|
|
# 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
|
|
|
|
|
# 67 DISPLAY W MATRIX
|
|
|
|
|
# 68
|
|
|
|
|
# 69 CAUSE RESTART
|
|
|
|
|
# 70 UPDATE LIFTOFF TIME
|
|
|
|
|
# 71 UNIVERSAL UPDATE-BLOCK ADR
|
|
|
|
|
# 72 UNIVERSAL UPDATE-SINGLE ADR
|
|
|
|
|
# 73 UPDATE AGC TIME (OCTAL)
|
|
|
|
|
# 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
|
|
|
|
|
# 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
|
|
|
|
|
# 76 MINIMUM IMPUSE COMMAND MODE.
|
|
|
|
|
# 77 RATE COMMAND AND ATTITUDE HOLD MODE
|
|
|
|
|
# 78 LR SPURIOUS RETURN TEST START (R77)
|
|
|
|
|
# 79 LR SPURIOUS RETURN TEST STOP
|
|
|
|
|
# 80 UPDATE LEM STATE VECTOR
|
|
|
|
|
# 81 UPDATE CSM STATE FECTOR
|
|
|
|
|
# 82 REQUEST ORBIT PARAM DISPLAY (R30)
|
|
|
|
|
# 83 REQUEST REND PARAM DISPLAY (R31)
|
|
|
|
|
# 84
|
|
|
|
|
# 85 DISPLAY RR LOS AZ AND ELEV
|
|
|
|
|
# 86
|
|
|
|
|
# 87
|
|
|
|
|
# Page 7
|
|
|
|
|
# 88
|
|
|
|
|
# 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
|
|
|
|
|
# 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
|
|
|
|
|
# 91 DISPLAY BANK SUM
|
|
|
|
|
# 92 OPERATE IMU PERFORMANCE TEST (P07)
|
|
|
|
|
# 93 ENABLE W MATRIX INITALIZATION
|
|
|
|
|
# 94
|
|
|
|
|
# 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
|
|
|
|
|
# 96 INTERRUPT INTEGRATION AND GO TO P00
|
|
|
|
|
# 97 PERFORM ENGINE FAIL PROCEDURE
|
|
|
|
|
# 98
|
|
|
|
|
# 99 PLEASE ENABLE ENGINE
|
|
|
|
|
|
|
|
|
|
# Page 8
|
|
|
|
|
# IN THE FOLLOWING NOUN LIST THE 'NO LOAD' RESTRICTION MEANS THE NOUN
|
|
|
|
|
# CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
|
|
|
|
|
# SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
|
|
|
|
|
# IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23
|
|
|
|
|
# MAY BE USED TO LOAD ANY OF THE NOUN'S COMPONENTS WHICH ARE NOT OF THE
|
|
|
|
|
# ABOVE SCALE TYPES.
|
|
|
|
|
#
|
|
|
|
|
# THE 'DEC ONLY' RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
|
|
|
|
|
# EVERY COMPONENT IN THE NOUN. (NOTE THAT 'NO LOAD' IMPLIES 'DEC ONLY'.)
|
|
|
|
|
|
|
|
|
|
# NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
|
|
|
|
|
# 00 NOT IN USE
|
|
|
|
|
# 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .xxxxx FOR EACH
|
|
|
|
|
# 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP xxxxx. FOR EACH
|
|
|
|
|
# 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP xxx.xx DEG FOR EACH
|
|
|
|
|
# 04 ANGULAR ERROR/DIFFERENCE 1COMP xxx.xx DEG
|
|
|
|
|
# 05 ANGULAR ERROR/DIFFERENCE 1COMP xxx.xx DEG
|
|
|
|
|
# 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
|
|
|
|
|
# LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
|
|
|
|
|
# 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
|
|
|
|
|
# ONES FOR BITS TO BE MODIFIED
|
|
|
|
|
# 1 TO SET OR 0 TO RESET SELECTED BITS
|
|
|
|
|
# 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
|
|
|
|
|
# 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
|
|
|
|
|
# 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
|
|
|
|
|
# 11 TIG OF CSI 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
|
|
|
|
|
# (USED BY EXTENDED VERBS ONLY)
|
|
|
|
|
# 13 TIG OF CDH 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 14 CHECKLIST 3COMP xxxxx. FOR EACH
|
|
|
|
|
# (USED BY EXTENDED VERBS ONLY)
|
|
|
|
|
# (NOUN 25 IS PASTED AFTER DISPLAY)
|
|
|
|
|
# 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
|
|
|
|
|
# 16 TIME OF EVENT 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# (USED BY EXTENDED VERBS ONLY) 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 17 SPARE
|
|
|
|
|
# 18 AUTO MANEUVER BALL ANGLES 3COMP xxx.xx DEG FOR EACH
|
|
|
|
|
# 19 SPARE
|
|
|
|
|
# 20 ICDU ANGLES 3COMP xxx.xx DEG FOR EACH
|
|
|
|
|
# 21 PIPAS 3COMP xxxxx. PULSES FOR EACH
|
|
|
|
|
# 22 NEW ICDU ANGLES 3COMP xxx.xx DEG FOR EACH
|
|
|
|
|
# 23 SPARE
|
|
|
|
|
# 24 DELTA TIME FOR AGC CLOCK 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# Page 9
|
|
|
|
|
# 25 CHECKLIST 3COMP xxxxx. FOR EACH
|
|
|
|
|
# (USED WITH PLEASE PERFORM ONLY)
|
|
|
|
|
# 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
|
|
|
|
|
# 27 SELF TEST ON/OFF SWITCH 1COMP xxxxx.
|
|
|
|
|
# 28 SPARE
|
|
|
|
|
# 29 SPARE
|
|
|
|
|
# 30 SPARE
|
|
|
|
|
# 31 SPARE
|
|
|
|
|
# 32 TIME FROM PERIGEE 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 33 TIME OF IGNITION 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 34 TIME OF EVENT 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 35 TIME FROM EVENT 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 36 TIME OF AGC CLOCK 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 37 TIG OF TPI 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 38 TIME OF STATE BEING INTEGRATED 3COMP 00xxx. HRS DEC ONLY
|
|
|
|
|
# 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 39 SPARE
|
|
|
|
|
|
|
|
|
|
# Page 10
|
|
|
|
|
# MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
|
|
|
|
|
# 40 TIME FROM IGNITION/CUTOFF 3COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
|
|
|
|
|
# VG, xxxx.x FT/SEC
|
|
|
|
|
# DELTA V (ACCUMULATED) xxxx.x FT.SEC
|
|
|
|
|
# 41 TARGET AZIMUTH 2COMP xxx.xx DEG (FOR SYSTEM TEST)
|
|
|
|
|
# ELEVATION xx.xxx DEG
|
|
|
|
|
# 42 APOGEE, 3COMP xxxx.x NAUT MI DEC ONLY
|
|
|
|
|
# PERIGEE, xxxx.x NAUT MI
|
|
|
|
|
# DELTA V (REQUIRED) xxxx.x FT/SEC
|
|
|
|
|
# 43 LATITUDE, 3COMP xxx.xx DEG DEC ONLY
|
|
|
|
|
# LONGITUDE, xxx.xx DEG
|
|
|
|
|
# ALTITUDE xxxx.x NAUT MI
|
|
|
|
|
# 44 APOGEE, 3COMP xxxx.x NAUT MI NO LOAD, DEC ONLY
|
|
|
|
|
# PERIGEE, xxxx.x NAUT MI
|
|
|
|
|
# TFF xxBxx MIN/SEC
|
|
|
|
|
# 45 MARKS, 3COMP xxxxx. NO LOAD, DEC ONLY
|
|
|
|
|
# TFI OF NEXT BURN, xxBxx MIN/SEC
|
|
|
|
|
# MGA xxx.xx DEG
|
|
|
|
|
# 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
|
|
|
|
|
# 47 LEM WEIGHT, 2COMP xxxxx. LBS DEC ONLY
|
|
|
|
|
# CSM WEIGHT xxxxx. LBS
|
|
|
|
|
# 48 GIMBAL PITCH TRIM, 2COMP xxx.xx DEG DEC ONLY
|
|
|
|
|
# GIMBAL ROLL TRIM xxx.xx DEG
|
|
|
|
|
# 49 DELTA R, 3COMP xxxx.x NAUT MI DEC ONLY
|
|
|
|
|
# DELTA V, xxxx.x FT/SEC
|
|
|
|
|
# RADAR DATA SOURCE CODE xxxxx.
|
|
|
|
|
# 50 SPARE
|
|
|
|
|
# 51 S-BAND ANTENNA ANGLES PITCH 2COMP xxx.xx DEG DEC ONLY
|
|
|
|
|
# YAW xxx.xx DEG
|
|
|
|
|
# 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP xxx.xx DEG
|
|
|
|
|
# 53 SPARE
|
|
|
|
|
# 54 RANGE, 3COMP xxx.xx NAUT MI DEC ONLY
|
|
|
|
|
# RANGE RATE, xxxx.x FT/SEC
|
|
|
|
|
# THETA xxx.xx DEG
|
|
|
|
|
# 55 NO. OF APSIDAL CROSSINGS 3COMP xxxxx. DEC ONLY
|
|
|
|
|
# ELEVATION ANGLE xxx.xx DEG
|
|
|
|
|
# CENTRAL ANGLE OF PASSIVE VEHICLE xxx.xx DEG
|
|
|
|
|
# 56 RR LOS AZIMUTH 2COMP xxx.xx DEG
|
|
|
|
|
# ELEVATION xxx.xx DEG
|
|
|
|
|
# 57 DELTA R 1COMP xxxx.x NAUT MI DEC ONLY
|
|
|
|
|
# 58 PERIGEE ALT (POST TPI) 3COMP xxxx.x NAUT MI DEC ONLY
|
|
|
|
|
# DELTA V TPI xxxx.x FT/SEC
|
|
|
|
|
# DELTA V TPF xxxx.x FT/SEC
|
|
|
|
|
# 59 DELTA VELOCITY LOS 3COMP xxxx.x FT/SEC FOR EA. DEC ONLY
|
|
|
|
|
# 60 HORIZONTAL VELOCITY 3COMP xxxx.x FT/SEC DEC ONLY
|
|
|
|
|
# ALTITUDE RATE xxxx.x FT/SEC
|
|
|
|
|
# COMPUTED ALTITUDE xxxxx. FEET
|
|
|
|
|
# 61 TIME TO GO IN BRAKING PHASE 3COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
|
|
|
|
|
# TIME FROM IGNITION xxBxx MIN/SEC
|
|
|
|
|
# Page 11
|
|
|
|
|
# CROSS RANGE DISTANCE xxxx.x NAUT MI
|
|
|
|
|
# 62 ABSOLUTE VALUE OF VELOCITY 3COMP xxxx.x FT/SEC NO LOAD, DEC ONLY
|
|
|
|
|
# TIME FROM IGNITION xxBxx MIN/SEC
|
|
|
|
|
# DELTA V (ACCUMULATED) xxxx.x FT/SEC
|
|
|
|
|
# 63 ABSOLUTE VALUE OF VELOCITY 3COMP xxxx.x FT/SEC DEC ONLY
|
|
|
|
|
# ALTITUDE RATE xxxx.x FT/SEC
|
|
|
|
|
# COMPUTED ALTITUDE xxxxx. FEET
|
|
|
|
|
# 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP xxBxx NO LOAD, DEC ONLY
|
|
|
|
|
# ALTITUDE RATE xxxx.x FT/SEC
|
|
|
|
|
# COMPUTED ALTITUDE xxxxx. FEET
|
|
|
|
|
# 65 SAMPLED AGC TIME 3COMP 00xxx. HRS. DEC ONLY
|
|
|
|
|
# (FETCHED IN INTERRUPT) 000xx. MIN MUST LOAD 3 COMPS
|
|
|
|
|
# 0xx.xx SEC
|
|
|
|
|
# 66 LR RANGE 2COMP xxxxx. FEET NO LOAD, DEC ONLY
|
|
|
|
|
# POSITION +0000x
|
|
|
|
|
# 67 LRVX 3COMP xxxxx. FT/SEC
|
|
|
|
|
# LRVY xxxxx. FT/SEC
|
|
|
|
|
# LRVZ xxxxx. FT/SEC
|
|
|
|
|
# 68 SLANT RANGE TO LANDING SITE 3COMP xxxx.x NAUT MI NO LOAD, DEC ONLY
|
|
|
|
|
# TIME TO GO IN BRAKING PHASE xxBxx MIN/SEC
|
|
|
|
|
# LR ALTITUDE - COMPUTED ALTITUDE xxxxx. FEET
|
|
|
|
|
# 69 SPARE
|
|
|
|
|
# 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
|
|
|
|
|
# 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
|
|
|
|
|
# 72 RR 360 - TRUNNION ANGLE 2COMP xxx.xx DEG
|
|
|
|
|
# SHAFT ANGLE xxx.xx DEG
|
|
|
|
|
# 73 NEW RR 360 - TRUNNION ANGLE 2COMP xxx.xx DEG
|
|
|
|
|
# SHAFT ANGLE xxx.xx DEG
|
|
|
|
|
# 74 TIME FROM IGNITION 3COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
|
|
|
|
|
# YAW AFTER VEHICLE RISE xxx.xx DEG
|
|
|
|
|
# PITCH AFTER VEHICLE RISE xxx.xx DEG
|
|
|
|
|
# 75 DELTA ALTITUDE CDH 3COMP xxxx.x NAUT MI NO LOAD, DEC ONLY
|
|
|
|
|
# DELTA TIME (CDH-CSI OR TPI-CDH) xxBxx MIN/SEC
|
|
|
|
|
# DELTA TIME (TPI-CDH OR TPI-NOMTPI) xxBxx MIN/SEC
|
|
|
|
|
# 76 DESIRED HORIZONTAL VELOCITY 3COMP xxxx.x FT/SEC DEC ONLY
|
|
|
|
|
# DESIRED RADIAL VELOCITY xxxx.x FT/SEC
|
|
|
|
|
# CROSS-RANGE DISTANCE xxxx.x NAUT MI
|
|
|
|
|
# 77 TIME TO ENGINE CUTOFF 2COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
|
|
|
|
|
# VELOCITY NORMAL TO CSM PLANE xxxx.x FT/SEC
|
|
|
|
|
# 78 RR RANGE 2COMP xxx.xx NAUT MI NO LOAD, DEC ONLY
|
|
|
|
|
# RANGE RATE xxxxx. FT/SEC
|
|
|
|
|
# 79 CURSOR ANGLE 3COMP xxx.xx DEG DEC ONLY
|
|
|
|
|
# SPIRAL ANGLE xxx.xx DEG
|
|
|
|
|
# POSITION CODE xxxxx.
|
|
|
|
|
# 80 DATA INDICATOR, 2COMP xxxxx.
|
|
|
|
|
# OMEGA xxx.xx DEG
|
|
|
|
|
# 81 DELTA V (LV) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
|
|
|
|
|
# Page 12
|
|
|
|
|
# 82 DELTA V (LV) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
|
|
|
|
|
# 83 DELTA V (BODY) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
|
|
|
|
|
# 84 DELTA V (OTHER VEHICLE) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
|
|
|
|
|
# 85 VG (BODY) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
|
|
|
|
|
# 86 VG (LV) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
|
|
|
|
|
# 87 BACKUP OPTICS LOS AZIMUTH 2COMP xxx.xx DEG
|
|
|
|
|
# ELEVATION xxx.xx DEG
|
|
|
|
|
# 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .xxxxx FOR EACH DEC ONLY
|
|
|
|
|
# 89 LANDMARK LATITUDE 3COMP xx.xxx DEG DEC ONLY
|
|
|
|
|
# LONGITUDE/2 xx.xxx DEC
|
|
|
|
|
# ALTITUDE xxx.xx NAUT MI
|
|
|
|
|
# 90 Y 3COMP xxx.xx NM DEC ONLY
|
|
|
|
|
# Y DOT xxxx.x FPS
|
|
|
|
|
# PSI xxx.xx DEG
|
|
|
|
|
# 91 ALTITUDE 3COMP xxxxxB. NAUT MI
|
|
|
|
|
# VELOCITY xxxxx. FT/SEC
|
|
|
|
|
# FLIGHT PATH ANGLE xxx.xx DEG
|
|
|
|
|
# 92 SPARE
|
|
|
|
|
# 93 DELTA GYRO ANGLES 3COMP xx.xxx DEG FOR EACH
|
|
|
|
|
# 94 SPARE
|
|
|
|
|
# 95 SPARE
|
|
|
|
|
# 96 SPARE
|
|
|
|
|
# 97 SYSTEM TEST INPUTS 3COMP xxxxx. FOR EACH
|
|
|
|
|
# 98 SYSTEM TEST RESULTS AND INPUTS 3COMP xxxxx.
|
|
|
|
|
# .xxxxx
|
|
|
|
|
# xxxxx.
|
|
|
|
|
# 99 RMS IN POSITION 3COMP xxxxx. FT DEC ONLY
|
|
|
|
|
# RMS IN VELOCITY xxxx.x FT/SEC
|
|
|
|
|
# RMS IN BIAS xx.xxx RADIANS
|
|
|
|
|
|
|
|
|
|
# Page 13
|
|
|
|
|
# REGISTERS AND SCALING FOR NORMAL NOUNS
|
|
|
|
|
|
|
|
|
|
# NOUN REGISTER SCALE TYPE
|
|
|
|
|
# 00 NOT IN USE
|
|
|
|
|
# 01 SPECIFY ADDRESS B
|
|
|
|
|
# 02 SPECIFY ADDRESS C
|
|
|
|
|
# 03 SPECIFY ADDRESS D
|
|
|
|
|
# 04 DSPTEM1 H
|
|
|
|
|
# 05 DSPTEM1 H
|
|
|
|
|
# 06 OPTION1 A
|
|
|
|
|
# 07 XREG A
|
|
|
|
|
# 08 ALMCADR A
|
|
|
|
|
# 09 FAILREG A
|
|
|
|
|
# 10 SPECIFY CHANNEL A
|
|
|
|
|
# 11 TCSI K
|
|
|
|
|
# 12 OPTIONX A
|
|
|
|
|
# 13 TCDH K
|
|
|
|
|
# 14 DSPTEMX C
|
|
|
|
|
# 15 INCREMENT ADDRESS A
|
|
|
|
|
# 16 DSPTEMX K
|
|
|
|
|
# 17 SPARE
|
|
|
|
|
# 18 FDAIX D
|
|
|
|
|
# 19 SPARE
|
|
|
|
|
# 20 CDUX D
|
|
|
|
|
# 21 PIPAX C
|
|
|
|
|
# 22 THETAD D
|
|
|
|
|
# 23 SPARE
|
|
|
|
|
# 24 DSPTEM2 +1 K
|
|
|
|
|
# 25 DSPTEM1 C
|
|
|
|
|
# 26 DSPTEM1 A
|
|
|
|
|
# 27 SMODE C
|
|
|
|
|
# 28 SPARE
|
|
|
|
|
# 29 SPARE
|
|
|
|
|
# 30 SPARE
|
|
|
|
|
# 31 SPARE
|
|
|
|
|
# 32 -TPER K
|
|
|
|
|
# 33 TIG K
|
|
|
|
|
# 34 DSPTEM1 K
|
|
|
|
|
# 35 TTOGO K
|
|
|
|
|
# 36 TIME2 K
|
|
|
|
|
# 37 TTPI K
|
|
|
|
|
# 38 TET K
|
|
|
|
|
# 39 SPARE
|
|
|
|
|
|
|
|
|
|
# Page 14
|
|
|
|
|
# REGISTERS AND SCALING FOR MIXED NOUNS
|
|
|
|
|
|
|
|
|
|
# NOUN COMP REGISTER SCALE TYPE
|
|
|
|
|
# 40 1 TTOGO L
|
|
|
|
|
# 2 VGDISP S
|
|
|
|
|
# 3 DVTOTAL S
|
|
|
|
|
# 41 1 DSPTEM1 D
|
|
|
|
|
# 2 DSPTEM1 +1 E
|
|
|
|
|
# 42 1 HAPO Q
|
|
|
|
|
# 2 HPER Q
|
|
|
|
|
# 3 VGDISP S
|
|
|
|
|
# 43 1 LAT H
|
|
|
|
|
# 2 LONG H
|
|
|
|
|
# 3 ALT Q
|
|
|
|
|
# 44 1 HAPOX Q
|
|
|
|
|
# 2 HPERX Q
|
|
|
|
|
# 3 TFF L
|
|
|
|
|
# 45 1 TRKMKCNT C
|
|
|
|
|
# 2 TTOGO L
|
|
|
|
|
# 3 +MGA H
|
|
|
|
|
# 46 1 DAPDATR1 A
|
|
|
|
|
# 47 1 LEMMASS KK
|
|
|
|
|
# 2 CSMMASS KK
|
|
|
|
|
# 48 1 PITTIME NN
|
|
|
|
|
# 2 ROLLTIME NN
|
|
|
|
|
# 49 1 R22DISP Q
|
|
|
|
|
# 2 R22DISP +2 S
|
|
|
|
|
# 3 WHCHREAD C
|
|
|
|
|
# 50 SPARE
|
|
|
|
|
# 51 1 ALPHASB H
|
|
|
|
|
# 2 BETASB H
|
|
|
|
|
# 52 1 ACTCENT H
|
|
|
|
|
# 53 SPARE
|
|
|
|
|
# 54 1 RANGE JJ
|
|
|
|
|
# 2 RRATE S
|
|
|
|
|
# 3 RTHETA H
|
|
|
|
|
# 55 1 NN C
|
|
|
|
|
# 2 ELEV H
|
|
|
|
|
# 3 CENTANG H
|
|
|
|
|
# 56 1 RR-AZ H
|
|
|
|
|
# 2 RR-ELEV H
|
|
|
|
|
# 57 1 DELTAR Q
|
|
|
|
|
# 58 1 POSTTPI Q
|
|
|
|
|
# 2 DELVTPI S
|
|
|
|
|
# 3 DELVTPF S
|
|
|
|
|
# 59 1 DVLOS S
|
|
|
|
|
# 2 DVLOS +2 S
|
|
|
|
|
# 3 DVLOS +4 S
|
|
|
|
|
# 60 1 VHORIZ S
|
|
|
|
|
# Page 15
|
|
|
|
|
# 2 HDOTDISP S
|
|
|
|
|
# 3 HCALC RR
|
|
|
|
|
# 61 1 TTFDISP L
|
|
|
|
|
# 2 TTOGO L
|
|
|
|
|
# 3 OUTOFPLN QQ
|
|
|
|
|
# 62 1 ABVEL S
|
|
|
|
|
# 2 TTOGO L
|
|
|
|
|
# 3 DVTOTAL S
|
|
|
|
|
# 63 1 ABVEL S
|
|
|
|
|
# 2 HDOTDISP S
|
|
|
|
|
# 3 HCALC1 RR
|
|
|
|
|
# 64 1 FUNNYDSP PP
|
|
|
|
|
# 2 HDOTDISP S
|
|
|
|
|
# 3 HCALC RR
|
|
|
|
|
# 65 1 SAMPTIME K
|
|
|
|
|
# 2 SAMPTIME K
|
|
|
|
|
# 3 SAMPTIME K
|
|
|
|
|
# 66 1 RSTACK +6 W
|
|
|
|
|
# 2 CHANNEL 33 TT
|
|
|
|
|
# 67 1 RSTACK X
|
|
|
|
|
# 2 RSTACK +2 Y
|
|
|
|
|
# 3 RSTACK +4 Z
|
|
|
|
|
# 68 1 RANGEDSP QQ
|
|
|
|
|
# 2 TTFDISP L
|
|
|
|
|
# 3 DELTAH RR
|
|
|
|
|
# 69 SPARE
|
|
|
|
|
# 70 1 AOTCODE A
|
|
|
|
|
# 2 AOTCODE +1 A
|
|
|
|
|
# 3 AOTCODE +2 A
|
|
|
|
|
# 71 1 AOTCODE A
|
|
|
|
|
# 2 AOTCODE +1 A
|
|
|
|
|
# 3 AOTCODE +2 A
|
|
|
|
|
# 72 1 CDUT WW
|
|
|
|
|
# 2 CDUS D
|
|
|
|
|
# 73 1 TANG WW
|
|
|
|
|
# 2 TANG +1 D
|
|
|
|
|
# 74 1 TTOGO L
|
|
|
|
|
# 2 YAW H
|
|
|
|
|
# 3 PITCH H
|
|
|
|
|
# 75 1 DIFFALT Q
|
|
|
|
|
# 2 T1TOT2 L
|
|
|
|
|
# 3 T2TOT3 L
|
|
|
|
|
# 76 1 ZDOTD S
|
|
|
|
|
# 2 RDOTD S
|
|
|
|
|
# 3 XRANGE Q
|
|
|
|
|
# 77 1 TTOGO L
|
|
|
|
|
# 2 YDOT S
|
|
|
|
|
# 78 1 RSTACK U
|
|
|
|
|
# 2 RSTACK +2 V
|
|
|
|
|
# 79 1 CURSOR D
|
|
|
|
|
# Page 16
|
|
|
|
|
# 2 SPIRAL D
|
|
|
|
|
# 3 POSCODE C
|
|
|
|
|
# 80 1 DATAGOOD C
|
|
|
|
|
# 2 OMEGAD H
|
|
|
|
|
# 81 1 DELVLVC S
|
|
|
|
|
# 2 DELVLVC +2 S
|
|
|
|
|
# 3 DELVLVC +4 S
|
|
|
|
|
# 82 1 DELVLVC S
|
|
|
|
|
# 2 DELVLVC +2 S
|
|
|
|
|
# 3 DELVLVC +4 S
|
|
|
|
|
# 83 1 DELVIMU S
|
|
|
|
|
# 2 DELVIMU +2 S
|
|
|
|
|
# 3 DELVIMU +4 S
|
|
|
|
|
# 84 1 DELVOV S
|
|
|
|
|
# 2 DELVOV +2 S
|
|
|
|
|
# 3 DELVOV +4 S
|
|
|
|
|
# 85 1 VGBODY S
|
|
|
|
|
# 2 VGBODY +2 S
|
|
|
|
|
# 3 VGBODY +4 S
|
|
|
|
|
# 86 1 DELVLVC S
|
|
|
|
|
# 2 DELVLVC +2 S
|
|
|
|
|
# 3 DELVLVC +4 S
|
|
|
|
|
# 87 1 AZ D
|
|
|
|
|
# 2 EL D
|
|
|
|
|
# 88 1 STARAD B
|
|
|
|
|
# 2 STARAD +2 B
|
|
|
|
|
# 3 STARAD +4 B
|
|
|
|
|
# 89 1 LANDLAT G
|
|
|
|
|
# 2 LANDLONG G
|
|
|
|
|
# 3 LANDALT JJ
|
|
|
|
|
# 90 1 RANGE JJ
|
|
|
|
|
# 2 RRATE S
|
|
|
|
|
# 3 RTHETA H
|
|
|
|
|
# 91 1 P21ALT Q (MEMORY/100 TO DISPLAY TENS N.M.)
|
|
|
|
|
# 2 P21VEL P
|
|
|
|
|
# 3 P21GAM H
|
|
|
|
|
# 92 SPARE
|
|
|
|
|
# 93 1 OGC G
|
|
|
|
|
# 2 OGC +2 G
|
|
|
|
|
# 3 OGC +4 G
|
|
|
|
|
# 94 SPARE
|
|
|
|
|
# 95 SPARE
|
|
|
|
|
# 96 SPARE
|
|
|
|
|
# 97 1 DSPTEM1 C
|
|
|
|
|
# 2 DSPTEM1 +1 C
|
|
|
|
|
# 3 DSPTEM1 +2 C
|
|
|
|
|
# 98 1 DSPTEM2 C
|
|
|
|
|
# 2 DSPTEM2 +1 B
|
|
|
|
|
# 3 DSPTEM2 +2 C
|
|
|
|
|
# 99 1 WWPOS XX
|
|
|
|
|
# Page 17
|
|
|
|
|
# 2 WWVEL YY
|
|
|
|
|
# 3 WWBIAS AAA
|
|
|
|
|
# Page 18
|
|
|
|
|
# NOUN SCALES AND FORMATS
|
|
|
|
|
|
|
|
|
|
# -SCALE TYPE- PRECISION
|
|
|
|
|
# UNITS DECIMAL FORMAT -- AGC FORMAT
|
|
|
|
|
# ------------ -------------- -- ----------
|
|
|
|
|
|
|
|
|
|
# -A-
|
|
|
|
|
# OCTAL xxxxx SP OCTAL
|
|
|
|
|
|
|
|
|
|
# -B- -14
|
|
|
|
|
# FRACTIONAL .xxxxx SP BIT 1 = 2 UNITS
|
|
|
|
|
# (MAX .99996)
|
|
|
|
|
|
|
|
|
|
# -C-
|
|
|
|
|
# WHOLE xxxxx. SP BIT 1 = 1 UNIT
|
|
|
|
|
# (MAX 16383.)
|
|
|
|
|
|
|
|
|
|
# -D- 15
|
|
|
|
|
# CDU DEGREES xxx.xx DEGREES SP BIT 1 = 360/2 DEGREES
|
|
|
|
|
# (MAX 359.99) (USES 15 BITS FOR MAGNI-
|
|
|
|
|
# TUDE AND 2-S COMP.)
|
|
|
|
|
|
|
|
|
|
# -E- 14
|
|
|
|
|
# ELEVATION DEGREES xx.xxx DEGREES SP BIT 1 = 90/2 DEGREES
|
|
|
|
|
# (MAX 89.999)
|
|
|
|
|
|
|
|
|
|
# -F- 14
|
|
|
|
|
# DEGREES (180) xxx.xx DEGREES SP BIT 1 = 180/2 DEGREES
|
|
|
|
|
# (MAX 179.99)
|
|
|
|
|
|
|
|
|
|
# -G-
|
|
|
|
|
# DP DEGREES (90) xx.xxx DEGREES DP BIT 1 OF LOW REGISTER =
|
|
|
|
|
# 28
|
|
|
|
|
# 360/2 DEGREES
|
|
|
|
|
|
|
|
|
|
# -H-
|
|
|
|
|
# DP DEGREES (360) xxx.xx DEGREES DP BIT 1 OF LOW REGISTER =
|
|
|
|
|
# 28
|
|
|
|
|
# (MAX 359.99) 360/2 DEGREES
|
|
|
|
|
|
|
|
|
|
# Page 19
|
|
|
|
|
# -K-
|
|
|
|
|
# TIME (HR, MIN, SEC) 00xxx. HR DP BIT 1 OF LOW REGISTER =
|
|
|
|
|
# 000xx. MIN -2
|
|
|
|
|
# 0xx.xx SEC 10 SEC
|
|
|
|
|
# (DECIMAL ONLY.
|
|
|
|
|
# MAX MIN COMP=59
|
|
|
|
|
# MAX SEC COMP=59.99
|
|
|
|
|
# MAX CAPACITY=745 HRS
|
|
|
|
|
# 39 MINS
|
|
|
|
|
# 14.55 SECS.
|
|
|
|
|
# WHEN LOADING, ALL 3
|
|
|
|
|
# COMPONENTS MUST BE
|
|
|
|
|
# SUPPLIED.)
|
|
|
|
|
|
|
|
|
|
# -L-
|
|
|
|
|
# TIME (MIN/SEC) xxBxx MIN/SEC DP BIT 1 OF LOW REGISTER =
|
|
|
|
|
# (B IS A BLANK -2
|
|
|
|
|
# POSITION, DECIMAL 10 SEC
|
|
|
|
|
# ONLY, DISPLAY OR
|
|
|
|
|
# MONITOR ONLY. CANNOT
|
|
|
|
|
# BE LOADED.
|
|
|
|
|
# MAX MIN COMP=59
|
|
|
|
|
# MAX SEC COMP=59
|
|
|
|
|
# VALUES GREATER THAN
|
|
|
|
|
# 59 MIN 59 SEC
|
|
|
|
|
# ARE DISPLAYED AS
|
|
|
|
|
# 59 MIN 59 SEC.)
|
|
|
|
|
|
|
|
|
|
# -M- -2
|
|
|
|
|
# TIME (SEC) xxx.xx SEC SP BIT 1 = 10 SEC
|
|
|
|
|
# (MAX 163.83)
|
|
|
|
|
|
|
|
|
|
# -N-
|
|
|
|
|
# TIME(SEC) DP xxx.xx SEC DP BIT 1 OF LOW REGISTER =
|
|
|
|
|
# -2
|
|
|
|
|
# 10 SEC.
|
|
|
|
|
|
|
|
|
|
# -P-
|
|
|
|
|
# VELOCITY 2 xxxxx. FEET/SEC DP BIT 1 OF HIGH REGISTER =
|
|
|
|
|
# (MAX 41994.) -7
|
|
|
|
|
# 2 METERS/CENTI-SEC
|
|
|
|
|
|
|
|
|
|
# -Q-
|
|
|
|
|
# POSITION 4 xxxx.x NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
|
|
|
|
|
# 2 METERS
|
|
|
|
|
|
|
|
|
|
# -S-
|
|
|
|
|
# VELOCITY 3 xxxx.x FT/SEC DP BIT 1 OF HIGH REGISTER =
|
|
|
|
|
# -7
|
|
|
|
|
# 2 METERS/CENTI-SEC
|
|
|
|
|
|
|
|
|
|
# Page 20
|
|
|
|
|
# -T- -2
|
|
|
|
|
# G xxx.xx G SP BIT 1 = 10 G
|
|
|
|
|
# (MAX 163.83)
|
|
|
|
|
|
|
|
|
|
# -U-
|
|
|
|
|
# RENDEZVOUS xxx.xx NAUT MI DP LOW ORDER BIT OF LOW ORDER
|
|
|
|
|
# RADAR RANGE WORD = 9.38 FEET
|
|
|
|
|
|
|
|
|
|
# -V-
|
|
|
|
|
# RENDEZVOUS xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
|
|
|
|
|
# RADAR RANGE RATE WORD = -.6278 FEET/SEC
|
|
|
|
|
|
|
|
|
|
# -W-
|
|
|
|
|
# LANDING RADAR xxxxx. FEET DP LOW ORDER BIT OF LOW ORDER
|
|
|
|
|
# ALTITUDE WORD = 1.079 FEET
|
|
|
|
|
|
|
|
|
|
# -X-
|
|
|
|
|
# LANDING RADAR xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
|
|
|
|
|
# VELX WORD = -.6440 FEET/SEC
|
|
|
|
|
|
|
|
|
|
# -Y-
|
|
|
|
|
# LANDING RADAR xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
|
|
|
|
|
# VELY WORD = 1.212 FEET/SEC
|
|
|
|
|
|
|
|
|
|
# -Z-
|
|
|
|
|
# LANDING RADAR xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
|
|
|
|
|
# VELZ WORD = .8668 FEET/SEC
|
|
|
|
|
|
|
|
|
|
# -AA-
|
|
|
|
|
# INITIAL/FINAL xxxxx. FEET DP LOW ORDER BIT OF LOW ORDER
|
|
|
|
|
# ALTITUDE WORD = 2.345 FEET
|
|
|
|
|
|
|
|
|
|
# -BB-
|
|
|
|
|
# ALTITUDE RATE xxxxx. FEET/SEC SP LOW ORDER BIT = .5
|
|
|
|
|
# (MAX 08191.) FEET/SEC
|
|
|
|
|
|
|
|
|
|
# -CC-
|
|
|
|
|
# FORWARD/LATERAL xxxxx. FEET/SEC SP LOW ORDER BIT = .5571
|
|
|
|
|
# VELOCITY (MAX 09126.) FEET/SEC
|
|
|
|
|
|
|
|
|
|
# -DD-
|
|
|
|
|
# ROTATIONAL HAND xxxxx. DEG/SEC SP FRACTIONAL PART OF PI RAD
|
|
|
|
|
# CONTROLLER ANGULAR (MAX 00044.) 4 SEC
|
|
|
|
|
# RATES
|
|
|
|
|
|
|
|
|
|
# -EE-
|
|
|
|
|
# OPTICAL TRACKER xxx.xx DEG. DP LOW ORDER BIT OF LOW ORDER
|
|
|
|
|
# AZIMUTH ANGLE 15
|
|
|
|
|
# WORD = 360/2 DEGREES
|
|
|
|
|
|
|
|
|
|
# Page 21
|
|
|
|
|
|
|
|
|
|
# -JJ-
|
|
|
|
|
# POSITION5 xxx.xx NAUT MI DP BIT 1 OF LOW REGISTER =
|
|
|
|
|
# 2 METERS
|
|
|
|
|
|
|
|
|
|
# -KK- 16
|
|
|
|
|
# WEIGHT2 xxxxx. LBS SP FRACTIONAL PART OF 2 KG
|
|
|
|
|
|
|
|
|
|
# -NN-
|
|
|
|
|
# TRIM DEGREES 2 xxx.xx DEG SP BIT 1=.01 SEC(TIME)
|
|
|
|
|
# (MAX 032.76)
|
|
|
|
|
|
|
|
|
|
# -PP-
|
|
|
|
|
# 2 INTEGERS +xxByy DP BIT 1 OF HIGH REGISTER =
|
|
|
|
|
# (B IS A BLANK 1 UNIT OF XX
|
|
|
|
|
# POSITION. DECIMAL BIT 1 OF LOW REGISTER =
|
|
|
|
|
# ONLY, DISPLAY OR 1 UNIT OF YY
|
2016-12-28 16:11:25 +00:00
|
|
|
# MONITOR ONLY. CANNOT (EACH REGISTER MUST
|
2016-07-31 22:32:55 +00:00
|
|
|
# BE LOADED.) CONTAIN A POSITIVE INTEGER
|
|
|
|
|
# (MAX 99B99) LESS THAN 100)
|
|
|
|
|
|
|
|
|
|
# -QQ-
|
|
|
|
|
# POSITION7 xxxx.x NAUT MI DP BIT 1 OF LOW REGISTER =
|
|
|
|
|
# (MAX 9058.9) -4
|
|
|
|
|
# 2 METERS
|
|
|
|
|
|
|
|
|
|
# -RR-
|
|
|
|
|
# COMPUTED ALTITUDE xxxxx. FEET DP BIT 1 OF LOW REGISTER =
|
|
|
|
|
# -4
|
|
|
|
|
# 2 METERS
|
|
|
|
|
|
|
|
|
|
# -SS-
|
|
|
|
|
# DP DEGREES xxxx.x DEGREES DP BIT 1 OF HIGH REGISTER =
|
|
|
|
|
# 1 DEGREE
|
|
|
|
|
|
|
|
|
|
# -TT-
|
|
|
|
|
# LANDING RADAR +0000x CHANNEL 33, BIT 6 = NOT POSIT. 1
|
|
|
|
|
# POSITION (DECIMAL ONLY. CHANNEL 33, BIT 7 = NOT POSIT. 2
|
|
|
|
|
# DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
|
|
|
|
|
# ONLY. CANNOT BE X = 2 FOR LR POSITION 2
|
|
|
|
|
# LOADED.)
|
|
|
|
|
|
|
|
|
|
# -WW- 15
|
|
|
|
|
# 360-CDU DEGREES xxx.xx DEGREES SP BIT 1 = 360 - (360/2 )
|
|
|
|
|
# (MAX 359.99) DEGREES
|
|
|
|
|
# (USES 15 BITS FOR MAGNI-
|
|
|
|
|
# TUDE AND 2-S COMP.)
|
|
|
|
|
|
|
|
|
|
# -XX-
|
|
|
|
|
# POSITION 9 xxxxx. FEET DP BIT 1 OF LOW REGISTER =
|
|
|
|
|
# -9
|
|
|
|
|
# 2 METERS
|
|
|
|
|
|
|
|
|
|
# Page 22
|
|
|
|
|
|
|
|
|
|
# -YY-
|
|
|
|
|
# VELOCITY 4 xxxx.x FEET/SEC DP FRACTIONAL PART
|
|
|
|
|
# (MAX 328.0) METERS/CENTI-SEC
|
|
|
|
|
|
|
|
|
|
# -AAA-
|
|
|
|
|
# RADIANS xx.xxx RADIANS DP BIT 1 OF HIGH REGISTER =
|
|
|
|
|
# (MAX 31.999) -9
|
|
|
|
|
# 2 RADIANS.
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
# THAT'S ALL ON THE NOUNS.
|
|
|
|
|
|
|
|
|
|
# Page 23
|
|
|
|
|
# ALARM CODES FOR LUMINARY
|
|
|
|
|
|
|
|
|
|
# *9 *18 *60 COLUMN
|
|
|
|
|
|
|
|
|
|
# CODE * TYPE SET BY
|
|
|
|
|
|
2016-12-28 16:11:25 +00:00
|
|
|
# 00105 ** AOTMARK SYSTEM IN USE
|
2016-07-31 22:32:55 +00:00
|
|
|
# 00107 MORE THAN 5 MARK PAIRS AOTMARK
|
|
|
|
|
# 00111 MARK MISSING AOTMARK
|
|
|
|
|
# 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
|
|
|
|
|
# 00113 NO INBITS AOTMARK
|
|
|
|
|
# 00114 MARK MADE BUT NOT DESIRED AOTMARK
|
|
|
|
|
# 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
|
|
|
|
|
# 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
|
|
|
|
|
# 00206 + GIMBAL LOC
|
|
|
|
|
# 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
|
|
|
|
|
# 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, RD2, P51, P57
|
|
|
|
|
# 00211 COARSE ALIGN ERROR IMU MODE SWITCH
|
|
|
|
|
# 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH, T4RPT
|
|
|
|
|
# 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
|
|
|
|
|
# 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
|
|
|
|
|
# 00217 BAD RETURN FROM IMUSTALL P51, P52, P57
|
|
|
|
|
# 00220 IMU NOT ALIGNED - NO REFSMMAT R02, R47
|
|
|
|
|
# 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
|
|
|
|
|
# FINDCDUW
|
|
|
|
|
# 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
|
|
|
|
|
# 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
|
|
|
|
|
# 00405 TWO STARS NOT AVAILABLE P52
|
|
|
|
|
# 00421 W-MATRIX OVERFLOW INTEGRV
|
|
|
|
|
# 00430 ** ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
|
|
|
|
|
# 00501 P RADAR ANTENNA OUT OF LIMITS R23
|
|
|
|
|
# 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
|
|
|
|
|
# 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
|
|
|
|
|
# 00510 RADAR AUTO DESCRETE NOT PRESENT R25
|
|
|
|
|
# 00511 LR NOT IN POSITION 2 OR REPOSITIONING SERVICER
|
|
|
|
|
# 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
|
|
|
|
|
# 00515 RR CDU FAIL DISCRETE PRESENT R25
|
|
|
|
|
# 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
|
|
|
|
|
# 00521 COULD NOT READ RADAR P20
|
|
|
|
|
# 00522 LANDING RADAR POSITION CHANGE RADAR READ
|
|
|
|
|
# 00523 P LR ANTENNA DIDN'T ACHIEVE POSITION 2 SERVICER, V60 (NON-P IN V60)
|
|
|
|
|
# 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
|
|
|
|
|
# 00526 P RANGE GREATER THAN 400 NAUT. MILES P20, P22
|
|
|
|
|
# 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21, R24
|
|
|
|
|
# LUNAR SURFACE
|
|
|
|
|
# OR VEHICLE MANEUVER REQUIRED R24 (20)
|
|
|
|
|
# 00530 P LOS NOT IN MODE2 COVERAGE R21
|
|
|
|
|
# ON LUNAR SURFACE AFTER 600 SECS.
|
|
|
|
|
# 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
|
|
|
|
|
# 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32, P72.
|
|
|
|
|
|
|
|
|
|
# Page 24
|
|
|
|
|
|
|
|
|
|
# 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32, P72.
|
|
|
|
|
# 00603 CSI TO CDH TIME LT TMIN12 P32, P72, P33, P73
|
2016-12-28 16:11:25 +00:00
|
|
|
# 00604 CDH TO TPI TIME LT TMIN23 P32, P72,
|
2016-07-31 22:32:55 +00:00
|
|
|
# OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
|
|
|
|
|
# 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
|
|
|
|
|
# 00606 DV EXCEEDS MAXIMUM P32, P72
|
|
|
|
|
# 00607 ** NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
|
|
|
|
|
# 00611 NO TIG FOR GIVEN ELEV ANGLE P34, P74
|
|
|
|
|
# 00701 ILLEGAL OPTION CODE SELECTED P57
|
|
|
|
|
# 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
|
|
|
|
|
# 01102 AGC SELF TEST ERROR SELF CHECK
|
|
|
|
|
# 01103 ** UNUSED CCS BRANCH EXECUTED ABORT
|
|
|
|
|
# 01104 * DELAY ROUTINE BUSY EXEC
|
|
|
|
|
# 01105 DOWNLINK TOO FAST T4RUPT
|
|
|
|
|
# 01106 UPLINK TOO FAST T4RUPT
|
|
|
|
|
# 01107 PHASE TABLE FAILURE. ASSUME RESTART
|
|
|
|
|
# ERASABLE MEMORY IS SUSPECT. RESTART
|
|
|
|
|
# 01201 * EXECUTIVE OVERFLOW - NO VAC AREAS EXEC
|
|
|
|
|
# 01202 * EXECUTIVE OVERFLOW - NO CORE SETS EXEC
|
|
|
|
|
# 01203 * WAITLIST OVERFLOW - TOO MANY TASKS WAITLIST
|
|
|
|
|
# 01204 ** WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
|
|
|
|
|
# CALLED WITH ZERO OR NEGATIVE DELTA-TIME
|
|
|
|
|
# 01206 ** SECOND JOB ATTEMPTS TO GO TO SLEEP PINBALL
|
|
|
|
|
# 01206 VIA KYBD AND DISPLAY PROGRAM
|
|
|
|
|
# 01207 * NO VAC AREAS FOR MARKS AOTMARK
|
|
|
|
|
# 01210 * TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
|
|
|
|
|
# 01211 * ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
|
|
|
|
|
# 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
|
|
|
|
|
# 01302 ** SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
|
|
|
|
|
# 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
|
|
|
|
|
# 01406 ** BAD RETURN FROM ROOTPSRS IGNITION ALGORITHM
|
|
|
|
|
#
|
|
|
|
|
# NOTE: 1406 IS A POODOO DURING THE IGNITION ALGORITHM
|
|
|
|
|
# AND AN ALARM DURING THE ACTUAL GUIDANCE PHASE.
|
|
|
|
|
#
|
|
|
|
|
# 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
|
|
|
|
|
# .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
|
|
|
|
|
# VECTOR.) S40.8
|
|
|
|
|
# 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
|
|
|
|
|
# 01412 DESCENT IGNALG NOT CONVERGING P63
|
|
|
|
|
# 01501 ** KEYBOARD AND DISPLAY ALARM DURING PINBALL
|
|
|
|
|
# 01501 INTERNAL USE (NVSUB). ABORT
|
|
|
|
|
# 01502 ** ILLEGAL FLASHING DISPLAY GOPLAY
|
|
|
|
|
# 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
|
|
|
|
|
# 01600 OVERFLOW IN DRIFT TEST IMU 4
|
|
|
|
|
# 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
|
|
|
|
|
# 01601 IMU 4 (LEM)
|
|
|
|
|
# 01703 IGNITION TIME SLIPPED MIDTOAVE
|
|
|
|
|
# 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
|
|
|
|
|
# CONFIGURATION P40, P42
|
|
|
|
|
|
|
|
|
|
# Page 25
|
|
|
|
|
|
|
|
|
|
# 02000 * DAP STILL IN PROGRESS AT NEXT TIMES RUPT DAP
|
|
|
|
|
# 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
|
|
|
|
|
# 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
|
|
|
|
|
# 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
|
|
|
|
|
# 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
|
|
|
|
|
# 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
|
|
|
|
|
# 04777 ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
|
|
|
|
|
# 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
|
|
|
|
|
# 10777 IMU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
|
|
|
|
|
# 13777 IMU, ICDU FAILS CAUSED THE ISS WARNING T4RUPT
|
|
|
|
|
# 14777 IMU, ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
|
|
|
|
|
#
|
|
|
|
|
# * INDICATES AN ABORT CODE THAT RESULTS IN A SOFTWARE RESTART.
|
|
|
|
|
#
|
|
|
|
|
# ** INDICATES A MORE SERIOUS ABORT CODE THAT RESULTS IN THE
|
|
|
|
|
# PROGRAM GOING TO R00.
|
|
|
|
|
#
|
|
|
|
|
# P INDICATES A PRIORITY ALARM.
|
|
|
|
|
#
|
|
|
|
|
# ALL OTHERS ARE NON-ABORTIVE
|
|
|
|
|
|
|
|
|
|
# Page 26
|
|
|
|
|
|
|
|
|
|
# CHECKLIST CODES FOR LUMINARY
|
|
|
|
|
|
|
|
|
|
# *9 *17 *26 *9 COLUMN
|
|
|
|
|
|
|
|
|
|
# R1CODE ACTION TO BE EFFECTED PROGRAM
|
|
|
|
|
|
|
|
|
|
# 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
|
|
|
|
|
# 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51, P63, P57
|
|
|
|
|
# 00014 ENTER DO LANDING SITE DETERMINATION (N89DISP) P57OPTION2
|
|
|
|
|
# 00015 PERFORM CELESTIAL BODY ACQUISITION R51, P51
|
|
|
|
|
# 00062 SWITCH AGC POWER DOWN P06
|
|
|
|
|
# 00201 SWITCH RR MODE TO AUTOMATIC P20, P22, R04
|
|
|
|
|
# 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12, P42, P71
|
|
|
|
|
# ALSO THR CONT TO AUTO P40, P63, P70
|
|
|
|
|
# 00205 PERFORM MANUAL ACQUISITION OF RR R23
|
|
|
|
|
# 00500 SWITCH LR ANTENNA TO POSITION 1 P63
|
|
|
|
|
|
|
|
|
|
# SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
|
|
|
|
|
# PERFORM DENOTES START OR END OF A TASK
|
|
|
|
|
# KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
|
|
|
|
|
|
|
|
|
|
# Page 27
|
|
|
|
|
# OPTION CODES FOR LUMINARY
|
|
|
|
|
|
|
|
|
|
# THE SPECIFIED OPTION CODES WIL BE FLASHED IN COMPONENT R1 IN
|
|
|
|
|
# CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
|
|
|
|
|
# ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
|
|
|
|
|
|
|
|
|
|
# *9 *17 *52 *11 *25 COLUMN
|
|
|
|
|
|
|
|
|
|
# OPTION
|
|
|
|
|
# CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
|
|
|
|
|
|
|
|
|
|
# 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
|
|
|
|
|
# 4=LAND SITE
|
|
|
|
|
# 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
|
|
|
|
|
# 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
|
|
|
|
|
# 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
|
|
|
|
|
# 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
|
|
|
|
|
# 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
|
|
|
|
|
# 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
|
|
|
|
|
# 2=TWO BODIES 3=ONE BODY + G
|
|
|
|
|
# 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
|
|
|
|
|
# ORBIT TO PASS OVER LM.
|
|
|
|
|
|
