Actuator placement from degree of controllability criteria for regular slewing of flexible spacecraft

DOI10.1016/0094-5765(81)90012-6zbMath0468.70030OpenAlexW2009947610MaRDI QIDQ3922246

Richard W. Longman, Kyle T. Alfriend

Publication date: 1981

Published in: Acta Astronautica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0094-5765(81)90012-6

zbMATH Keywords

degree of controllabilityvibrations of flexible spacecraft

Mathematics Subject Classification ID

Controllability (93B05) Astronomy and astrophysics (85A99) Orbital mechanics (70M20)

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