A dual-wheel multi-mode spacecraft actuator for near-minimum-time large angle slew maneuvers

DOI10.1016/J.AST.2008.01.003zbMath1273.70044OpenAlexW1986515921MaRDI QIDQ2853531

Willem H. Steyn

Publication date: 22 October 2013

Published in: Aerospace Science and Technology (Search for Journal in Brave)

Full work available at URL: http://www.sciencedirect.com/science/article/pii/S1270963808000217

zbMATH Keywords

control moment gyrosatellite attitude controlsingularity avoidanceeigenaxis slewminimum-time maneuvers

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Orbital mechanics (70M20)

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