DocumentCode
2416379
Title
Nonlinear regulation in halo orbits control design
Author
Di Giamberardino, P. ; Monaco, S.
Author_Institution
Dipartimento di Inf. e. Sistemistica, Rome Univ., Italy
fYear
1992
fDate
1992
Firstpage
536
Abstract
The design and simulation of feedback control laws for tracking prescribed quasi-halo orbits around the translunar libration point L 2 in the Earth-Moon system are considered. The nonlinear regulation approach is used to design control laws for asymptotically tracking those trajectories. The eccentricity of the system is considered and modeled by a periodic disturbance. Simulation with saturations on the controls validates the proposed strategies, which also give good results for large orbital maneuvers
Keywords
aerospace control; artificial satellites; feedback; nonlinear control systems; position control; Earth-Moon system; feedback control laws; halo orbits control design; nonlinear regulation; orbital maneuvers; periodic disturbance; quasi-halo orbits; translunar libration point; Control design; Control theory; Ear; Earth; Equations; Feedback control; Mathematical model; Orbits; Satellites; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1992., Proceedings of the 31st IEEE Conference on
Conference_Location
Tucson, AZ
Print_ISBN
0-7803-0872-7
Type
conf
DOI
10.1109/CDC.1992.371676
Filename
371676
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