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Modeling And Control Of Spacecraft Systems With Coupled Orbital And Attitude Dynamics

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posted on 08.06.2021, 12:46 by Alexander Frias
Spacecraft formation flying with coupled orbital-attitude dynamics is one of the most intriguing topics in the field of astronautics. Orbital-attitude coupling is induced when a non-symmetrical spacecraft in orbit is disturbed by means of active maneuvering or by external disturbances. Direct contributing factors to the coupled dynamics include the orbital radius, the gravitational parameter and the orbital angular velocity. Disturbance due to coupling is inherently weak in nature (in the order of magnitudes of 10





Aerospace Engineering

Granting Institution

Ryerson University