Article ID Journal Published Year Pages File Type
1715193 Acta Astronautica 2012 15 Pages PDF
Abstract
► Mixed H∞/H2 control for trajectory-tracking of rendezvous is investigated. ► Actuator faults and exogenous disturbances are taken into account. ► Parameter-dependent Lyapunov functions are adopted to reduce conservatism. ► Slack matrices are introduced to further reduce conservatism. ► A hybrid genetic algorithm is presented to obtain the desired controller.
Related Topics
Physical Sciences and Engineering Engineering Aerospace Engineering
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