Title :
Nonlinear regulation in halo orbits control design
Author :
Di Giamberardino, P. ; Monaco, S.
Author_Institution :
Dipartimento di Inf. e. Sistemistica, Rome Univ., Italy
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;
Conference_Titel :
Decision and Control, 1992., Proceedings of the 31st IEEE Conference on
Conference_Location :
Tucson, AZ
Print_ISBN :
0-7803-0872-7
DOI :
10.1109/CDC.1992.371676
