MANEUVER AND VIBRATION CONTROL OF HYBRID COORDINATE SYSTEMS USING LYAPUNOV STABILITY THEORY

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In this study, we present a generalized control law design methodology that covers a large class of systems, especially flexible structures described by hybrid discrete/distributed coordinate systems. The Lyapunov stability theory is used to develop globally stabilizing control laws. A hybrid version of Hamilton's canonical equations is introduced, which provides a direct path to designing stabilizing control laws for general nonlinear hybrid systems. The usual loss of robustness due to model reduction is overcome by this Lyaponov approach, which does not require truncation of the flexible systems into finite dimensional discrete systems.
Publisher
AMER INST AERONAUT ASTRONAUT
Issue Date
1993
Language
English
Article Type
Article
Citation

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.16, no.4, pp.668 - 676

ISSN
0731-5090
DOI
10.2514/3.21066
URI
http://hdl.handle.net/10203/66449
Appears in Collection
AE-Journal Papers(저널논문)
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