# Copyright: Public domain. # Filename: GIMBAL_LOCK_AVOIDANCE.agc # Purpose: Part of the source code for Comanche, build 055. # It is part of the source code for the Command Module's (CM) # Apollo Guidance Computer (AGC), Apollo 11. # Assembler: yaYUL # Reference: pp. 412-413 # Contact: Onno Hommes <ohommes@cmu.edu>. # Website: www.ibiblio.org/apollo. # Mod history: 05/07/09 OH Transcription Batch 1 Assignment # # The contents of the "Comanche055" files, in general, are transcribed # from scanned documents. # # Assemble revision 055 of AGC program Comanche by NASA # 2021113-051. April 1, 1969. # # This AGC program shall also be referred to as Colossus 2A # # Prepared by # Massachusetts Institute of Technology # 75 Cambridge Parkway # Cambridge, Massachusetts # # under NASA contract NAS 9-4065. # # Refer directly to the online document mentioned above for further information. # Please report any errors to info@sandroid.org.
# Page 412 BANK15 SETLOC KALCMON1 BANK
EBANK= BCDU # DETECTING GIMBAL LOCK
LOCSKIRT EQUALS WCALC
WCALC LXC,1DLOAD*
RATEINDX
ARATE,1
SR4 CALL# COMPUTE THE INCREMENTAL ROTATION MATRIX
DELCOMP # DEL CORRESPONDING TO A 1 SEC ROTATION # ABOUT COF DLOAD* VXSC
ARATE,1
COF
MXV
QUADROT STODL BRATE
AM
DMP DDV*
ANGLTIME
ARATE,1
SR 5 STOVL TM
BRATE VXSC
BIASCALE STORE BIASTEMP # ATTITUDE ERROR BIAS TO PREVENT OVERSHOOT # IN SYSTEM
SETGO # STATE SWITCH CALCMAN2 (43D)
CALCMAN2 # 0(OFF) = BYPASS STARTING PROCEDURE
NEWANGL +1# 1(ON) = START MANEUVER
ARATE 2DEC .0022222222# = .05 DEG/SEC
2DEC .0088888889# = .2 DEG/SEC
2DEC .0222222222# = .5 DEG/SEC
2DEC .0888888889# = 2 DEG/SEC $22.5 DEG/SEC
ANGLTIME 2DEC .000190735# = 100B - 19
# MANEUVER ANGLE TO MANEUVER TIME
QUADROT 2DEC .1# ROTATION MATRIX FROM S/C AXES TO CONTROL
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