Add IMU and Gyro Drift Rates and Accelerometer Biases #1030
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IMU drift compensation from the CMC, showing NBDX,Y,Z ADIAX,Y,Z and ADSRAX,Y,Z combined. CMC is compensating for NBD before, and after an 1800 ft/sec SPS burn, and compensating for all nine drift rates during the burn. All three axes have been tested separately to confirm sign and handedness in the CM/CMC. on to the LM... |
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Testing State vector for Apollo 11 Launch
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#1247 can you add this to your branch to prevent merge conflicts with OO? Just update the LM padcount for Apollo 10 and add those two addresses zeroed, think it makes it 200 for yours |
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just need to resolve the merge conflict on the Apollo 10 LM pads that you got from pulling the main branch |
Should be fixed now. |
... NASSP/Apollo - Mission Scenarios/Apollo 10/Apollo 10 - 10 - Before Undocking T+98h15min.scn
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...lo - NASSP/Apollo - Mission Scenarios/Apollo 10/Apollo 10 - 12 - Before Phasing TIG-6min.scn
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...pollo - NASSP/Apollo - Mission Scenarios/Apollo 9/Apollo 9 - 33 - Before Entry Interface.scn
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...P/Apollo - Mission Scenarios/Apollo 11/Apollo 11 - 17 - Before Lunar Liftoff T+124h20min.scn
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The CMC padload here reverses the changes that were done for switching from Comanche 55 to 67.
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I think this may have been the result of a bad merge-conflict resolution on my part.
...lo - NASSP/Apollo - Mission Scenarios/Apollo 10/Apollo 10 - 12 - Before Phasing TIG-6min.scn
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...- NASSP/Apollo - Mission Scenarios/Apollo 10/Apollo 10 - 13 - Before Insertion TIG-11min.scn
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Bugfixes to AGC IMU bias compensation in Apollo 9 and 10 mission scen…
This is very much WIP. Adding so it doesn't get lost.