Stability analysis of flexible spacecraft with PID controller / by J. de Lafontaine.: Co24-3/7-1372-1984E-PDF

"This study presents a graphical method for the design and analysis of a flexible spacecraft controller. It can handle as many modes as desired, in constrained or unconstrained form;modal separability is not assumed and the method is exact when the spacecraft axes are uncoupled. The definition of a 'system function', independent of the controller parameters, simplifies the determination of the system stability boundaries. It also allows the investigation of the modal separability assumption, resulting in a criterion for its validity. Stabilization through structural damping and flexible modes filtering is illustrated using graphs of the system function. Closed-form approximations are derived in order to complement the exact, numerical method. Extensions to systems with loop delay andnonlinear elements are also included along with applications to the LSAT-1 Roll axis"--Abstract.

Permanent link to this Catalogue record:
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Publication information
Department/Agency Communications Research Centre (Canada), issuing body.
Title Stability analysis of flexible spacecraft with PID controller / by J. de Lafontaine.
Series title CRC report ; no. 1372
Publication type Series - View Master Record
Language [English]
Format Electronic
Electronic document
Note(s) "Space Technology and Applications Branch."
"November 1984."
Digitized edition from print [produced by Innovation, Science and Economic Development Canada].
Includes bibliographical references (page 53).
Publishing information Ottawa : Communications Research Centre, 1984.
Author / Contributor De Lafontaine, J., author.
Description 1 online resource (viii, 55 pages) : illustrations.
Catalogue number
  • Co24-3/7-1372-1984E-PDF
Subject terms PID controllers.
Expandable space structures.
Space vehicles -- Control systems.
Stability of space vehicles.
Régulateurs PID.
Structures flexibles.
Véhicules spatiaux -- Systèmes de commande.
Vaisseaux spatiaux -- Stabilité.
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