LGC Programmes , Luminary 1D.
Number Title
Service
P00 LGC Idling
P06 PGNCS Power
P07 Systems Test (Non-flight)
Ascent
P12 Powered Ascent Guidance
Coast
P20 Rendezvous Navigation
P21 Ground Track Determination
P22 RR Lunar Surface Navigation
P25 Preferred Tracking Attitude
P27 LGC Update
Pre-thrusting
P30 External delta-V
P32 Co-elliptic Sequence Initiation (CSI)
P33 Constant Delta Altitude (CDH)
P34 Transfer Phase Initiation (TPI)
P35 Transfer Phase Midcourse (TPM)
Thrust
P40 DPS Thrusting
P41 RCS Thrusting
P42 APS Thrusting
P47 Thrust Monitor
Alignments
P51 IMU Orientation Determination
P52 IMU Realign
P57 Lunar Surface Alignment
Descent & Landing
P63 Landing Maneuvre Braking Phase
P64 Landing Maneuvre Approach Phase
P66 Rate of Descent Landing (ROD)
P68 Landing Confirmation
Aborts & Backups
P70 DPS Abort
P71 APS Abort
P72 CSM Co-elliptic Sequence Initiation (CSI) Targeting
P73 CSM Constant Delta Altitude (CDH) Targeting
P74 CSM Transfer Phase Initiation (TPI) Targeting
P75 CSM Transfer Phase Midcourse (TPM) Targeting
P76 Target delta V.
Verb codes
05 Display Octal Components 1, 2, 3 in R1, R2, R3.
06 Display Decimal (Rl or R1, R2 or R1, R2, R3)
25 Load Component 1, 2, 3 into R1, R2, R3.
27 Display Fixed Memory
37 Change Programme (Major Mode)
47 Initialise AGS (R47)
48 Request DAP Data Load Routine (RO3)
49 Request Crew Defined Maneuvre Routine (R62)
50 Please Perform
54 Mark X or Y reticle
55 Increment LGC Time (Decimal)
57 Permit Landing Radar Updates
59 Command LR to Position 2
60 Display Vehicle Attitude Rates (FDAI)
63 Sample Radar Once per Second (R04)
69 Cause Restart
71 Universal Update, Block Address (P27)
75 Enable U, V Jets Firing During DPS Burns
76 Minimum Impulse Command Mode (DAP)
77 Rate Command and Attitude Hold Mode (DAP)
82 Request Orbit Parameter Display (R30)
83 Request Rendezvous Parameter Display (R31)
97 Perform Engine Fail Procedure (R40)
99 Please Enable Engine Ignition
Noun Codes
11 TIG of CSI
13 TIG of CDH
16 Time of Event
18 Auto Maneuvre to FDAI Ball Angles
24 Delta Time for LGC Clock
32 Time from Perigee
33 Time of Ignition
34 Time of Event
35 Time from Event
36 Time of LGC Clock
37 Time of Ignition of TPI
40 (a) Time from Ignition/Cutoff
(b) VG
(c) Delta V (Accumulated)
41 Target Azimuth and Target Elevation
42 (a) Apogee Altitude
(b) Perigee Altitude
(c) Delta V (Required)
43 (a) Latitude (+North)
(b) Longitude (+East)
(c) Altitude
44 (a) Apogee Altitude
(b) Perigee Altitude
(c) TFF
45 (a) Marks
(b) TFI of Next/Last Burn
(c) MGA
54 (a) Range
(b) Range Rate
(c) Theta
61 (a) TGO in Braking Phase
(b) TFI
(c) Cross Range Distance
65 Sampled LGC Time
66 LR Slant Range and LR Position
68 (a) Slant Range to Landing Site
(b) TGO in Braking Phase
(c) LR Altitude-computed altitude
69 Landing Site Correction, Z, Y and X
76 (a) Desired Horizontal Velocity
(b) Desired Radial Velocity
(c) Cross-Range Distance
89 (a) Landmark Latitude (+N)
(b)Longitude/2 (+E)
(c)Altitude
92 (a) Desired Thrust Percentage of DPS
(b) Altitude Rate
(c) Computed Altitude
CGC Programmes (Skylab SL-11, CM-116)
Pre-launch & Service
P00 CMC Idling
P01 Pre-launch or service initialisation
P02 Pre-launch or service - gyro compassing
P03 Pre-launch or service - optical verification of gyro compassing
P06 GNCS Power down
PO7 Systems Test
Boost/Coast
P11 Earth orbit insertion monitor (EOI)
P20 Universal tracking
P21 Ground track determination
P25 Contingency VHF Range-Rate
P27 CMC Update
P29 Time-to-longitude
Pre-thrust Targeting
P30 External delta-V
P31 First phasing maneuvre (NC1)
P32 Second phasing maneuvre (NC2)
P33 Corrective combination maneuvre (NCC)
P34 Co-elliptic maneuvre(NSR)
P35 Transfer Phase Initiation (TPI)
P36 Transfer Phase Midcourse (TPM)
P37 Rendezvous Final Phase
P38 Plane Change (PC)
Thrusting
P40 SPS
P41 RCS
P47 Thrust Monitor
P48 Rendezvous thrust monitor
Alignment
P50 ATM Orientation determination
P51 IMU Orientation determination
P52 IMU Realign
P53 Back-up IMU orientation determination
P54 Back-up IMU realign
P55 ATM star tracker gimbal angles
Entry
P61 Entry preparation
P62 Entry CM/SM separation and pre-entry maneuvre
P63 Entry initialisation
P64 Entry-Post 0.05g
P65 Entry-Up control
P66 Entry-ballistics
P67 Entry-Final phase
Post Thrusting
P77 CSM Velocity vector updating






