Turn over Problem of Tether Satellite System
Author:
Affiliation:
1. Tokyo Metropolitan University, Japan
2. Tokyo Metropolitan Institute of Technology, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.IAC-05-C1.P.24
Reference5 articles.
1. Deployment/retrieval control of tethered subsatellite through an optimal path
2. Mission function control of tethered subsatellite deployment/retrieval - In-plane and out-of-plane motion
3. Trajectory Analysis for Deployment / Retrieval of Tethered Subsatellite Using Metric' JGCDVol.26, No.1, Jan.Feb., 2003, pp.177-179.
4. Analysis Approach to Minimum Energy Maneuver Problems for Flexible Space Structures," AIAA Journal of Guidance, Control, and Dynamics, Vol.25, No.6,Nov.Dec. 2002, pp.1136-1142.
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