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Virginia Polytechnic Institute and State University

Time optimal slewing of flexible spacecraft

Abstract

dc:description.abstract

The time optimal slewing problem for flexible spacecraft is considered. We study single-axis rotational maneuvers for a simple flexible system, consisting of a rigid hub with an elastic appendage. The equations of motions are derived by Hamilton’s Principle, and a discrete nonlinear model is obtained by the assumed modes method. The problem is first solved in a discrete linearized space by parameter optimization. Optimality is verified by Pontryagin’s Maximum Principle. The linear solutions are then used to obtain time optimal solutions for the non-linear problem by a multiple-shooting algorithm. Although this approach is applicable to arbitrary boundary conditions, this work is confined, almost exclusively, to rest-to-rest maneuvers. These maneuvers are shown to possess some interesting symmetric and asymptotic properties. The problem is further analyzed in infinite-dimensional space, and the convergence of the finite-dimensional approximations is studied. Finally, a soft version of the time optimal slewing problem is considered, where the control is bounded only by a penalty term in the cost functional. A perturbation technique is applied to further simplify this problem.

Degree

thesis:*
Name thesis:degree_name
Ph. D.
Level thesis:degree_level
doctoral
Discipline thesis:degree_discipline
Aerospace and Ocean Engineering
Department dc:contributor.department
Aerospace and Ocean Engineering
Grantor dc:publisher
Virginia Polytechnic Institute and State University
Year dc:date.issued
1988

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Ben-Asher, Joseph Z.
Chair dc:contributor.committeechair
  • Cliff, Eugene M.
Committee members dc:contributor.committeemember
  • Burns, John A.
  • Lutze, Frederick H.
  • Haftka, Raphael T.
  • Bingulac, Stanoje
  • Herdman, Terry L.

Rights

dc:rights
Statement dc:rights
  • In Copyright
Language dc:language.iso
en_US

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/10919/53910
OAI identifier oai:identifier
oai:vtechworks.lib.vt.edu:10919/53910

Chain of custody

source
Harvested from
Virginia Tech
Base URL
vtechworks.lib.vt.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
related terms
citation

Ben-Asher, Joseph Z.. Time optimal slewing of flexible spacecraft. doctoral thesis, Virginia Polytechnic Institute and State University, 1988. http://hdl.handle.net/10919/53910