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Controlling Chaotic Attitude Motion of Spacecraft by the Input‐Output Linearization
Author(s) -
Chen L.Q.,
Liu Y.Z.
Publication year - 2000
Publication title -
zamm ‐ journal of applied mathematics and mechanics / zeitschrift für angewandte mathematik und mechanik
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.449
H-Index - 51
eISSN - 1521-4001
pISSN - 0044-2267
DOI - 10.1002/1521-4001(200010)80:10<701::aid-zamm701>3.0.co;2-y
Subject(s) - spacecraft , chaotic , control theory (sociology) , linearization , motion (physics) , orbit (dynamics) , feedback linearization , nonlinear system , gravitational field , physics , drag , computer science , control (management) , mathematics , classical mechanics , aerospace engineering , mechanics , engineering , artificial intelligence , astronomy , quantum mechanics
In this paper, the control of chaotic oscillations is investigated. A nonlinear control methodology termed input‐output linearization is utilized. Chaotic attitude motion of a spacecraft moving on an elliptic orbit in the gravitational field with both air drag and internal damping is treated as an example.