Simple processors of star tracker commands for stabilizing an inertially oriented satellite
By: by Robert D. Showman, Brian F. Doolin, and G. Michael Sullivan
Contributors: Doolin, Brian F.; Sullivan, G. Michael; Ames Research Center; United States. National Aeronautics and Space Administration
Series: NASA technical note -- NASA TN D-4490; NASA technical note -- D-4490
Publisher: National Aeronautics and Space Administration; For sale by the Clearinghouse for Federal Scientific and Technical Information
Published: 1968
Place of publication: Washington, D.C; Springfield, Va
Language: eng
Number of pages: 62
Subjects: Artificial satellites; Attitude control systems; Mathematical models; Stellar inertial navigation systems
Notes: "March 1968"--Cover.

Prepared at Ames Research Center.

Includes bibliographical references (p. 58).