An optimal slewing maneuver approach for a class of spacecraft with flexible appendages

DOI10.1016/0094-5765(86)90086-XzbMath0603.70030MaRDI QIDQ3740317

Keiichi Hirako, Isao Yamaguchi, Yoshiaki Ohkami, Takashi Kida, Hiroshi Soga

Publication date: 1986

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

zbMATH Keywords

maximum principleattitude maneuvering problemopen- loop control of the rigid body modesrobust feedback control of the elastic vibration modespacecraft with flexible appendages

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

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