"Position and attitude control of a spacecraft using the state-dependent ..."

Donald T. Stansbery, James R. Cloutier (2000)

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DOI: 10.1109/ACC.2000.879525

access: closed

type: Conference or Workshop Paper

metadata version: 2023-04-29

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Donald T. Stansbery, James R. Cloutier:
Position and attitude control of a spacecraft using the state-dependent Riccati equation technique. ACC 2000: 1867-1871

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