An optimal slewing maneuver approach for a class of spacecraft with flexible appendages (Q3740317)
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| Language | Label | Description | Also known as |
|---|---|---|---|
| English | An optimal slewing maneuver approach for a class of spacecraft with flexible appendages |
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An optimal slewing maneuver approach for a class of spacecraft with flexible appendages (English)
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1986
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attitude maneuvering problem
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spacecraft with flexible appendages
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open- loop control of the rigid body modes
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maximum principle
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robust feedback control of the elastic vibration mode
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