Flight Trajectory and Control System of SELenological and Engineering Explorer "KAGUYA" mission to the Moon
Author:
Affiliation:
1. Japan Aerospace Exploration Agency
2. NEC Aerospace Systems
3. NEC TOSHIBA Space Systems
4. NEC Co.
5. Mitsubishi Space Software Co.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7483
Reference16 articles.
1. Berry, R. L. "Launch window and translunar, Iunar orbit, and transearth trajectory planning and control for the Apollo11 Iunar landing mission,"AIAA-1970-24,1970.
2. Japanese first double lunar swingby mission “Hiten”
3. Lozier, D., Galal, K., Folta, D., and Beckman, M. "LUNAR PROSPECTOR MISSION DESIGN AND TRAJECTORY SUPPORT,"AAS98-323,1998.
4. Gestal,D.,Camino,O.,andetal."SMART-1OPERATIONS,"IAC-05-B5.3/B5.5,2005.
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