The effects of structural flexibility on the nonlinear attitude control of spacecraft
By: by Tarek Mohamed Mohamed Abdel-Rahman.
Contributors: Toronto, Ont. University.
Publisher: s.n.]
Published: 1977
Place of publication: [Toronto
Language: eng
Number of pages: 356
Subjects: Space vehicles -- Attitude control systems; Space vehicles -- Control systems
Notes: Thesis--University of Toronto.

Vita.

Includes bibliographies.