This paper proposes two different methods of estimating the disturbance torque imparted on the Cassini spacecraft by its MEA cover actuator, using attitude control flight data.
Trending Main Engine Assembly (MEA) Cover Actuator Performance Using Cassini Attitude Control Flight Data
AIAA Sci Tech 2016: Guidance, Navigation and Control (GNC) Conference ; 2016 ; San Diego, CA, United States
04.01.2016
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 2016
|The Cassini Main Engine Assembly Cover Mechanism
NTRS | 1997
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