Scenario File Options: Difference between revisions
imported>Mark Grant (Try a table instead) |
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The '''Project Apollo''' scenarios have a vast number of options that you can specify. Some of the more useful are: | The '''Project Apollo''' scenarios have a vast number of options that you can specify. Some of the more useful are: | ||
==General options== | |||
These are options specifying things such as the fuel mass, the intended orbit after launch, etc. | |||
{|border = "1" | {|border = "1" | ||
!width="100"|Option || Function | !width="100"|Option || Function | ||
|- | |||
|TOAPO||Specifies the desired launch apogee altitude in kilometers. | |||
|- | |||
|TOPER||Specifies the desired launch perigee altitude in kilometers. | |||
|- | |||
|TOHDG||Specifies the desired launch azimuth in degrees. | |||
|- | |- | ||
|DLS||Set to 1 to delete the launch site when the spacecraft passes out of visible range. This can give a significant performance boost on slow machines. | |DLS||Set to 1 to delete the launch site when the spacecraft passes out of visible range. This can give a significant performance boost on slow machines. | ||
|- | |||
|FDAIDISABLED||Set to 1 to disable the OpenGL FDAI rendering. This can give a significant performance boost on slow machines. | |||
|- | |- | ||
|IGMST||Inertial Guidance Mode start: set to the time in seconds after launch at which the autopilot switches to inertial guidance mode and starts trying to hit the target orbit rather than follow the pre-planned pitch program. | |IGMST||Inertial Guidance Mode start: set to the time in seconds after launch at which the autopilot switches to inertial guidance mode and starts trying to hit the target orbit rather than follow the pre-planned pitch program. | ||
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8 Docking adapter for an SIVb 'wet workshop'<BR> | 8 Docking adapter for an SIVb 'wet workshop'<BR> | ||
</code> | </code> | ||
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|} | |||
==AGC options== | |||
AGC options are specified between AGC_BEGIN and AGC_END. Options outside those lines will be ignored. | |||
{|border = "1" | |||
!width="100"|Option || Function | |||
|- | |||
|YAAGC||Set to 1 to use the Virtual AGC rather than the C++ AGC | |||
|- | |||
|EMEM||Set an AGC erasable memory location to a specified value. Addresses and values are both specified in octal (base-8), so to set address 10 (decimal) to 17 (decimal) you would specify <code>EMEM0012 21</code>. In general you should use LMPAD and CMPAD instead of specifying specific memory locations as both C++ AGC and Virtual AGC use the same scenario values to store different data. | |||
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* [[Config File Options]] | * [[Config File Options]] | ||
[[Category:Scenario configuration]] | [[Category:Scenario configuration]] |
Revision as of 01:44, 31 October 2006
The Project Apollo scenarios have a vast number of options that you can specify. Some of the more useful are:
General options
These are options specifying things such as the fuel mass, the intended orbit after launch, etc.
Option | Function |
---|---|
TOAPO | Specifies the desired launch apogee altitude in kilometers. |
TOPER | Specifies the desired launch perigee altitude in kilometers. |
TOHDG | Specifies the desired launch azimuth in degrees. |
DLS | Set to 1 to delete the launch site when the spacecraft passes out of visible range. This can give a significant performance boost on slow machines. |
FDAIDISABLED | Set to 1 to disable the OpenGL FDAI rendering. This can give a significant performance boost on slow machines. |
IGMST | Inertial Guidance Mode start: set to the time in seconds after launch at which the autopilot switches to inertial guidance mode and starts trying to hit the target orbit rather than follow the pre-planned pitch program. |
SIFUELMASS |
Specifies the mass in kilograms of the fuel in the first stage (SIc or SIb). |
SIEMPTYMASS |
Specifies the empty mass in kilograms of the first stage (SIc or SIb). |
SIIFUELMASS |
Specifies the mass in kilograms of the fuel in the second stage (SIVb for Saturn 1b or SII for Saturn V). This is not used for the INT-20. |
SIIEMPTYMASS |
Specifies the empty mass in kilograms of the second stage (SIVb for Saturn 1b or SII for Saturn V). This is not used for the INT-20. |
S4FUELMASS |
Specifies the mass in kilograms of the fuel in the SIVb stage of Saturn V and derivatives. |
S4PL |
Specifies the payload of the SIVb stage. Current values are:
|
AGC options
AGC options are specified between AGC_BEGIN and AGC_END. Options outside those lines will be ignored.
Option | Function |
---|---|
YAAGC | Set to 1 to use the Virtual AGC rather than the C++ AGC |
EMEM | Set an AGC erasable memory location to a specified value. Addresses and values are both specified in octal (base-8), so to set address 10 (decimal) to 17 (decimal) you would specify EMEM0012 21 . In general you should use LMPAD and CMPAD instead of specifying specific memory locations as both C++ AGC and Virtual AGC use the same scenario values to store different data.
|