Combined control of fast attitude maneuver and stabilization for large complex spacecraft

DOI10.1007/S10409-013-0080-8zbMath1346.70032OpenAlexW1972291295MaRDI QIDQ318000

Yao Zhang, Jing-Rui Zhang

Publication date: 4 October 2016

Published in: Acta Mechanica Sinica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10409-013-0080-8

zbMATH Keywords

path planningattitude controlvibration suppressioninput shaping

Mathematics Subject Classification ID

Application models in control theory (93C95) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

Cites Work

• Influence of flexible solar arrays on vibration isolation platform of control moment gyroscopes
• A dual-wheel multi-mode spacecraft actuator for near-minimum-time large angle slew maneuvers

This page was built for publication: Combined control of fast attitude maneuver and stabilization for large complex spacecraft