Mission File Options: Difference between revisions

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(Add more mission file parameters)
(Add more parameters)
 
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|CMtoLMPowerConnectionVersion||CM to LM power connection version. 0 = connection doesn't work with LM staged, 1 = LM has a CB to bypass circuit to descent stage, 2 = circuit bypassed automatically at staging.||0
|CMtoLMPowerConnectionVersion||CM to LM power connection version. 0 = connection doesn't work with LM staged, 1 = LM has a CB to bypass circuit to descent stage, 2 = circuit bypassed automatically at staging.||0
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|EmptySMCG||Center-of-gravity of the empty SM (but including SM RCS) in inches||914.5916, -6.6712, 12.2940
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|HasRateAidedOptics||FALSE = Optics mode switch is not bypassed for CMC to optics commands, TRUE = optics mode switch is bypassed for CMC to optics commands (ECP 792)||FALSE
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|CrossPointerReversePolarity||FALSE = Normal polarity (Apollo 14 and earlier), TRUE = Lateral axis for PGNS and LR input has switched polarity (Apollo 15 and later)||FALSE
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|CrossPointerShades||FALSE = No shades (Apollo 15 and earlier), TRUE = Shades (Apollo 16 & 17)||FALSE
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|LMNumber||Get LM number for mission specific EPS, ECS and CWEA versions. In the future this will also decide which systems config file will be loaded||5
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|LMEventTimerReverseAtZero||FALSE= LM event timer continues to count down through zero, TRUE = when reaching zero it starts counting up (Apollo 13 and later)||FALSE
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|Apollo13Failures||Run special Apollo 13 failure and audio code||FALSE
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|CDRVesselName||Name of CDR, used for EVA vessel||CDR
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|CMPVesselName||Name of CMP, used for EVA vessel||CMP
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|LMPVesselName||Name of LMP, used for EVA vessel||LMP
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|CDRSuitName||Name of CDR to print on suit||CDR
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|CMPSuitName||Name of CMP to print on suit||CMP
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|LMPSuitName||Name of LMP to print on suit||LMP
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|CSMDefaultCueCards||If set to FALSE then none of the default CSM cue cards are shown ||TRUE
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|LMDefaultCueCards||If set to FALSE then none of the default LM cue cards are shown ||TRUE
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|CSMCueCard||Adds a mission specific cue card. Format example: "CSMCueCard=1 SATURN_BOOST_A15" adds the cue card with the mesh name SATURN_BOOST_A15 to card location 1 in the CSM.||
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|LMCueCard||Adds a mission specific cue card. Format example: "LMCueCard=1 EXAMPLE_CARD" adds the cue card with the mesh name EXAMPLE_CARD to card location 1 in the LM.||
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|CMPIPABIASX||CM PIPA X-axis bias in cm/sec^2||0.0
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|CMPIPASCALEX||CM PIPA X-axis scale factor in ppm||0.0
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|CMPIPABIASY||CM PIPA Y-axis bias in cm/sec^2||0.0
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|CMPIPASCALEY||CM PIPA Y-axis scale factor in ppm||0.0
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|CMPIPABIASZ||CM PIPA Z-axis bias in cm/sec^2||0.0
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|CMPIPASCALEZ||CM PIPA Z-axis scale factor in ppm||0.0
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|CMNBDX||CM IRIG X-axis gyro bias drift in meru||0.0
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|CMNBDY||CM IRIG Y-axis gyro bias drift in meru||0.0
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|CMNBDZ||CM IRIG Z-axis gyro bias drift in meru||0.0
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|CMADIAX||CM IRIG X-axis gyro drift due to acceleration in the input axis in meru/g||0.0
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|CMADIAY||CM IRIG Y-axis gyro drift due to acceleration in the input axis in meru/g||0.0
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|CMADIAZ||CM IRIG Z-axis gyro drift due to acceleration in the input axis in meru/g||0.0
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|CMADSRAX||CM IRIG X-axis gyro drift due to acceleration in the spin axis in meru/g||0.0
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|CMADSRAY||CM IRIG Y-axis gyro drift due to acceleration in the spin axis in meru/g||0.0
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|CMADSRAZ||CM IRIG Z-axis gyro drift due to acceleration in the spin axis in meru/g||0.0
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|LMPIPABIASX||LM PIPA X-axis bias in cm/sec^2||0.0
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|LMPIPASCALEX||LM PIPA X-axis scale factor in ppm||0.0
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|LMPIPABIASY||LM PIPA Y-axis bias in cm/sec^2||0.0
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|LMPIPASCALEY||LM PIPA Y-axis scale factor in ppm||0.0
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|LMPIPABIASZ||LM PIPA Z-axis bias in cm/sec^2||0.0
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|LMPIPASCALEZ||LM PIPA Z-axis scale factor in ppm||0.0
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|LMNBDX||LM IRIG X-axis gyro bias drift in meru||0.0
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|LMNBDY||LM IRIG Y-axis gyro bias drift in meru||0.0
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|LMNBDZ||LM IRIG Z-axis gyro bias drift in meru||0.0
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|LMADIAX||LM IRIG X-axis gyro drift due to acceleration in the input axis in meru/g||0.0
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|LMADIAY||LM IRIG Y-axis gyro drift due to acceleration in the input axis in meru/g||0.0
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|LMADIAZ||LM IRIG Z-axis gyro drift due to acceleration in the input axis in meru/g||0.0
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|LMADSRAX||LM IRIG X-axis gyro drift due to acceleration in the spin axis in meru/g||0.0
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|LMADSRAY||LM IRIG Y-axis gyro drift due to acceleration in the spin axis in meru/g||0.0
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|LMADSRAZ||LM IRIG Z-axis gyro drift due to acceleration in the spin axis in meru/g||0.0
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TBD
TBD

Latest revision as of 15:27, 25 June 2026

NASSP uses a mission file to specify vehicle configuration and mission parameters.

Option Function Default Value
SMJCVersion Service Module Jettison Controller version. A modification was used on Apollo 13 and later to prevent the Service Module from skipping out of the atmosphere on reentry. Valid values are:

1 Block I and pre Apollo 13
2 Apollo 13 and later

1
JMission If set to TRUE, the CSM will have the panels and systems that were flown on the J-type Apollo missions FALSE
Panel277Version Version of CSM panel 277. Valid values are:

0 No panel
1 J-type mission panel
2 Skylab missions panel

0
Panel278Version Version of CSM panel 278. Valid values are:

1 Pre Apollo 15
2 Apollo 15-16
3 Apollo 17
4 Skylab
5 ASTP

1
LMDSKYVersion Version of the LM DSKY. Valid values are:

1 Same as CM DSKY (Apollo 10 and before)
2 ALT and VEL lights (Apollo 11-14)
3 PRIO DISP and NO DAP lights (Apollo 15-17)

2
HasLMProgramer If set to TRUE the Lunar Module Programer for automatic flight and remote control is used (Apollo 5 only) FALSE
HasAEA If set to TRUE the Lunar Module has an Abort Electronics Assembly (computer of the AGS). Only Apollo 5 did not fly one. TRUE
LMHasAscEngArmAssy If set to TRUE the Ascent Engine Arming Assembly is used to remotely fire the APS engine in an unmanned configuration (flown on Apollo 9 and 10). FALSE
LMHasLegs If set to TRUE then the LM has legs. TRUE
LMHasDeflectors If set to TRUE then the LM has RCS plume deflectors. TRUE
LMHasCask If set to TRUE then the LM has a RTG Cask. TRUE
CSMHasHGA If set to TRUE then the CSM has an S-Band High Gain Antenna. TRUE
CSMHasVHFRanging If set to TRUE then the CSM has the VHF Ranging System. TRUE
CMCVersion Name of the CMC software. Artemis072
TEPHEM0 If Skylark or a custom CMC rope is used for the mission, this value is used to initialize the CMC clock on initial startup. It is the MJD at midnight July 1st preceeding the launch. 41133.0
LGCVersion Name of the LGC software. Luminary210
AEAVersion Name of the AEA software. FP8
InvertLMStageBit Input bit to the LGC software for the current stage (descent stage attached or not) is inverted. This was the case on Apollo 5 (LM-1) FALSE
ATCA_PRM_Factor A factor used in the LM ATCA to control the linearity of the ACA inputs for rotational control by the astronauts. Apollo 9 used 0.1 which was determined to be too sensitive, so that it got changed to 0.3 afterwards 0.3
LM_CGX_Coefficients Polynomial coefficients for the LM ascent stage center-of-gravity X-component as a function of total mass. 8.7719e-08, -7.9329e-04, 7.9773e+00
LM_CGY_Coefficients Polynomial coefficients for the LM ascent stage center-of-gravity Y-component as a function of total mass. 2.1488e-10, -2.5485e-06, 1.2769e-02
LM_CGZ_Coefficients Polynomial coefficients for the LM ascent stage center-of-gravity Z-component as a function of total mass. 6.1788e-09, -6.9019e-05, 2.5186e-01
CMtoLMPowerConnectionVersion CM to LM power connection version. 0 = connection doesn't work with LM staged, 1 = LM has a CB to bypass circuit to descent stage, 2 = circuit bypassed automatically at staging. 0
EmptySMCG Center-of-gravity of the empty SM (but including SM RCS) in inches 914.5916, -6.6712, 12.2940
HasRateAidedOptics FALSE = Optics mode switch is not bypassed for CMC to optics commands, TRUE = optics mode switch is bypassed for CMC to optics commands (ECP 792) FALSE
CrossPointerReversePolarity FALSE = Normal polarity (Apollo 14 and earlier), TRUE = Lateral axis for PGNS and LR input has switched polarity (Apollo 15 and later) FALSE
CrossPointerShades FALSE = No shades (Apollo 15 and earlier), TRUE = Shades (Apollo 16 & 17) FALSE
LMNumber Get LM number for mission specific EPS, ECS and CWEA versions. In the future this will also decide which systems config file will be loaded 5
LMEventTimerReverseAtZero FALSE= LM event timer continues to count down through zero, TRUE = when reaching zero it starts counting up (Apollo 13 and later) FALSE
Apollo13Failures Run special Apollo 13 failure and audio code FALSE
CDRVesselName Name of CDR, used for EVA vessel CDR
CMPVesselName Name of CMP, used for EVA vessel CMP
LMPVesselName Name of LMP, used for EVA vessel LMP
CDRSuitName Name of CDR to print on suit CDR
CMPSuitName Name of CMP to print on suit CMP
LMPSuitName Name of LMP to print on suit LMP
CSMDefaultCueCards If set to FALSE then none of the default CSM cue cards are shown TRUE
LMDefaultCueCards If set to FALSE then none of the default LM cue cards are shown TRUE
CSMCueCard Adds a mission specific cue card. Format example: "CSMCueCard=1 SATURN_BOOST_A15" adds the cue card with the mesh name SATURN_BOOST_A15 to card location 1 in the CSM.
LMCueCard Adds a mission specific cue card. Format example: "LMCueCard=1 EXAMPLE_CARD" adds the cue card with the mesh name EXAMPLE_CARD to card location 1 in the LM.
CMPIPABIASX CM PIPA X-axis bias in cm/sec^2 0.0
CMPIPASCALEX CM PIPA X-axis scale factor in ppm 0.0
CMPIPABIASY CM PIPA Y-axis bias in cm/sec^2 0.0
CMPIPASCALEY CM PIPA Y-axis scale factor in ppm 0.0
CMPIPABIASZ CM PIPA Z-axis bias in cm/sec^2 0.0
CMPIPASCALEZ CM PIPA Z-axis scale factor in ppm 0.0
CMNBDX CM IRIG X-axis gyro bias drift in meru 0.0
CMNBDY CM IRIG Y-axis gyro bias drift in meru 0.0
CMNBDZ CM IRIG Z-axis gyro bias drift in meru 0.0
CMADIAX CM IRIG X-axis gyro drift due to acceleration in the input axis in meru/g 0.0
CMADIAY CM IRIG Y-axis gyro drift due to acceleration in the input axis in meru/g 0.0
CMADIAZ CM IRIG Z-axis gyro drift due to acceleration in the input axis in meru/g 0.0
CMADSRAX CM IRIG X-axis gyro drift due to acceleration in the spin axis in meru/g 0.0
CMADSRAY CM IRIG Y-axis gyro drift due to acceleration in the spin axis in meru/g 0.0
CMADSRAZ CM IRIG Z-axis gyro drift due to acceleration in the spin axis in meru/g 0.0
LMPIPABIASX LM PIPA X-axis bias in cm/sec^2 0.0
LMPIPASCALEX LM PIPA X-axis scale factor in ppm 0.0
LMPIPABIASY LM PIPA Y-axis bias in cm/sec^2 0.0
LMPIPASCALEY LM PIPA Y-axis scale factor in ppm 0.0
LMPIPABIASZ LM PIPA Z-axis bias in cm/sec^2 0.0
LMPIPASCALEZ LM PIPA Z-axis scale factor in ppm 0.0
LMNBDX LM IRIG X-axis gyro bias drift in meru 0.0
LMNBDY LM IRIG Y-axis gyro bias drift in meru 0.0
LMNBDZ LM IRIG Z-axis gyro bias drift in meru 0.0
LMADIAX LM IRIG X-axis gyro drift due to acceleration in the input axis in meru/g 0.0
LMADIAY LM IRIG Y-axis gyro drift due to acceleration in the input axis in meru/g 0.0
LMADIAZ LM IRIG Z-axis gyro drift due to acceleration in the input axis in meru/g 0.0
LMADSRAX LM IRIG X-axis gyro drift due to acceleration in the spin axis in meru/g 0.0
LMADSRAY LM IRIG Y-axis gyro drift due to acceleration in the spin axis in meru/g 0.0
LMADSRAZ LM IRIG Z-axis gyro drift due to acceleration in the spin axis in meru/g 0.0

TBD

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