Abstract
The automatical rendezvous and dock for two spacecrafts are very complex job in aerostro technology. The attitute and range of the target spacecraft relative to active spacecraft must be measure.(1) Becouse of the blind zone of microwave radar the laser radar sensor must be use in short range measuring. In the paper, a method measured attitute angle of the target spacecraft has been introduced. The method is based on "tilted effect" by the narrow interference filter.
© 1991 Optical Society of America
PDF ArticleMore Like This
Stephen Adelman, Frederik Weindling, and Dane O. Lowrey
TUC2 Conference on Laser and Electrooptical Systems (CLEO:S&I) 1976
Dai Yongjiang, Wu Haibin, and Yang Xuedong
ME5 Coherent Laser Radar (CLR) 1991
J.F. Shanley, F.J. Weaver, S.J. Caputi, and A.R. Reisinger
ME1 Coherent Laser Radar (CLR) 1991