IMAN is a Python tool that provides inertial sensor-based estimates of spacecraft trajectories within an atmospheric influence. It provides Kalman filter-derived spacecraft state estimates based upon data collected onboard, and is shown to perform at a level comparable to the conventional methods of spacecraft navigation in terms of accuracy and at a higher level with regard to the availability of results immediately after completion of an atmospheric drag pass.
Inertial Measurements for Aero-assisted Navigation (IMAN)
01.09.2007
Sonstige
Keine Angabe
Englisch
Inertial measurements for aerobraking navigation (IMAN)
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