Attitude manoeuvre of spacecraft with long cantilever beam appendage by momentum wheel

DOI10.1080/00207179.2012.733029zbMath1278.93140OpenAlexW2091156004MaRDI QIDQ2871718

Dandan Yang, Bao-Zeng Yue

Publication date: 9 January 2014

Published in: International Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207179.2012.733029

zbMATH Keywords

active controlmomentum wheelresidual nutation angleappendagesteady state timeattitude manoeuvreresidual transversal angular velocity

Mathematics Subject Classification ID

Control/observation systems governed by partial differential equations (93C20) Feedback control (93B52)

Related Items (1)

Investigation on attitude disturbance control and vibration suppression for fuel-filled flexible spacecraft

Cites Work

• Chaotic attitude and reorientation maneuver for completely liquid-filled spacecraft with flexible appendage
• Study on the global chaotic dynamics and control of liquid-filled spacecraft with flexible appendage
• Feedback Control Law Design for the Dual-Spin Turn of Spacecraft
• Spinup dynamics of gyrostats

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