Attitude control of a satellite in an elliptic orbit.
نویسندگان
چکیده
منابع مشابه
An efficient method to control the amplitude of the limit cycle in satellite attitude control system
In this paper, an efficient method is presented to control the attitude of a satellite with ON-OFF actuator. The main objective of this novel method is to control the amplitude of the limit cycle which commonly appears in the steady state of such systems; and at the same time by consideration of real actuator constraints, reduce the fuel consumption of system. The Proposed method is a combinati...
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ژورنال
عنوان ژورنال: Journal of Spacecraft and Rockets
سال: 1967
ISSN: 0022-4650,1533-6794
DOI: 10.2514/3.28883