toutatis < With this file LUT will be in English.
Thanks Art Blos...
But English can be a pain when you have to learn words that you will never use in normal day to day life.
but in my life... Never...
Code: Select all
"Mars Reconnaissance Orbiter:MRO:2005-029A" "Sol"
{
Class "spacecraft"
Mesh "mars-reconnaissance-orbiter.cmod"
Radius 0.0065
Timeline
[
{
Beginning 2453595.029166667 #
Ending 2453805.0 #
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{
EclipticJ2000 { Center "Sol" }
}
SampledTrajectory
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Interpolation "cubic"
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BodyFrame
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}
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Ending 2453896.5 #
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Ending 2454353.5 #
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Ending 2454444.5 #
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Ending 2454535.5 #
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Ending 2454627.5 #
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Ending 2454719.5 #
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Ending 2454810.5 #
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}
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FixedRotation
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Ending 2454992.5 #
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}
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Ending 2455084.5 #
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Ending 2455175.5 #
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Ending 2455265.5 #
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Ending 2455357.5 #
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Ending 2455449.5 #
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Ending 2455540.5 #
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Ending 2455630.5 #
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Ending 2455722.5 #
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Ending 2455814.5 #
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Ending 2455905.5 #
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Ending 2456271.5 #
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Ending 2456545.5 #
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Ending 2456636.5 #
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Ending 2456726.5 #
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Ending 2456910.5 #
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Yes, Sirius_Alpha... that is right...inclination changes occur best at lower orbital velocities. Inclination changes at apoastron are much more fuel-efficient since the components of the velocity vector are smaller.
I'm not sure I understand exactly what you mean. Are you saying that because the inclination change was performed at apoastron, you think the data is suspecft?