Attitude stability and performance of a dual-spin satellite with large flexible appendages
By: D. B. Cherchas.
Contributors: UTIAS
Series: UTIAS report -- no.170
Publisher: Institute for Aerospace Studies
Published: 1971
Place of publication: [Downsview, Ont.]
Subjects: Attitude stability; Dual spin spacecraft; Solar arrays
Notes: Includes bibliographical refrences.