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Issue:
Optimal Control of Orbit Maintenance and Maneuver
Author(s):
Han Chao\ Fu Hongxun Beijing University of Aeronautics and Astronautics
,
Beijing 100083
Pages:
40
-
46
Year:
2000
Issue:
4
Journal:
Aerospace Control
Keyword:
Spacecraft\ Orbital keeping\ Orbital maneuver\ Optimal control
;
Abstract:
This paper provides a new optimal control method for orbital maintenance and maneuver,which begins with the kinetics equation of spacecraft and is based on the linear discrete optimal control theory,establishes the relative optimal control model and gives its solution.The simulation results show that the given optimal control method in this paper is correct and feasible.
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