Multi-Objective Trajectory Optimization by a Hierarchical Gradient Algorithm with Fuzzy Decision Logic-Application to Slew Maneuver Problems of a Flexible Space Structure-
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Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/51/598/51_598_589/_pdf
Reference23 articles.
1. Near-minimum time, closed-loop slewing of flexible spacecraft
2. Time-optimal slewing of flexible spacecraft
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4. Minimum-time control characteristics of flexible structures
5. Closed-loop soft-constrained time-optimal control of flexible space structures
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1. H.INF. Tracking Control for Minimum Time Slewing of Flexible Space Structure;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2005
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