Three-axis stabilization of spacecraft using parameter-independent nonlinear quaternion feedback
By: Suresh M. Joshi, Atul G. Kelkar.
Contributors: Kelkar, Atul, 1963-; Langley Research Center.
Series: NASA technical memorandum -- 109150.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1994
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Attitude control.; Attitude stability.; Control systems design.; Feedback control.; Nonlinear feedback.; Quaternions.; Spacecraft control.
Other titles: Three axis stabilization of spacecraft using parameter-independent nonlinear quaternion feedback.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0276-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.