Guidance and navigation system design of R-bar approach for rendezvous and docking

17th AIAA International Communications Satellite Systems Conference and Exhibit

Volumn , Issue , 1998, Pages

  Yamanaka, Koji ^a   Yokota, Kiyomi ^a   Yamada, Katsuhiko ^b   Yoshikawa, Shoji ^b   Koyama, Hiroshi ^b   Tsukahara, Katsumi ^b   Nakamura, Taichi ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b MITSUBISHI ELECTRIC CORPORATION   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE CONTROL; COMMUNICATION SATELLITES; MANNED SPACE FLIGHT; NAVIGATION SYSTEMS; ORBITS;

ATTITUDE SENSORS; GPS SIGNALS; POSITIONAL ACCURACY; QUICK APPROACH; RELATIVE NAVIGATION; RENDEZVOUS AND DOCKING;

AIR NAVIGATION;

EID: 84930915255     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-1299     Document Type: Conference Paper

References (4)

1. Kunugi, M., Koyama, H. and Nakamura, T.: Guidance, Navigation and Control System in Engineering Test Satellite VII Rendezvous and Docking Experiment, IFAC Symposium on Automatic Control in Aerospace, 1994.
2. Kawano, I., Koyama, H. and et al.: Flight Control and Management Strategies of Rendezvous & Docking System for ETS-VII,19th International Symposium on Space Technology and Science,1994.
3. Nishimura, T., Kanai, K., and Murata, M.: Control and guidance in aerospace, pp. 256-257, SICE, Tokyo, 1995 (in Japanese).
4. Takeuchi K: Mathematical Statistics, pp. 96-100, Touyoukeizai-Shinpousha, Tokyo, 1963 (in Japanese).