Format:
Online-Ressource (XIV, 141 pp)
,
digital
Edition:
Reproduktion Springer eBook Collection. Engineering
ISBN:
9783540409441
Series Statement:
Lecture Notes in Control and Information Sciences 221
Content:
Addressing the difficult problem of controlling flexible spacecraft having multiple articulated appendages is the aim of this volume. Such systems are needed for space mission concepts including multi-payload space platforms and autonomous space-based manipulators. These systems are characterised by highly nonlinear dynamics, flexibility in members and joints, low inherent damping, and modeling uncertainty. A complete nonlinear rotational dynamic model of a generic multibody flexible system is derived, and is shown to possess certain passivity properties. The main result is a class of passivity-based nonlinear and linear output feedback control laws that enable globally stable closed-loop manoeuvres. The control laws are robust to parametric uncertainties, unmodeled uncertainties, and in some cases, actuator and sensor nonlinearities. All results given are also applicable to flexible terrestrial manipulators
Note:
Literaturverz. S. [129] - 137
Additional Edition:
ISBN 9783540760931
Additional Edition:
Erscheint auch als Druck-Ausgabe Kelkar, Atul G. Control of nonlinear multibody flexible space structures London : Springer, 1996 ISBN 3540760938
Language:
English
Subjects:
Mathematics
Keywords:
Raumfahrzeug
;
Mehrkörpersystem
;
Dynamisches Verhalten
;
Regelung
URL:
Volltext
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