Attitude stabilization of a pico-satellite by momentum wheel and magnetic coils

DOI10.1631/JZUS.A0820425zbMath1206.93087OpenAlexW1979667456MaRDI QIDQ621433

Zhong-He Jin, Hao Wang, Ke Han, Tao Meng

Publication date: 2 February 2011

Published in: Journal of Zhejiang University. Science A (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1631/jzus.a0820425

zbMATH Keywords

attitude controlmagnetic coilsmomentum wheelpico-satellite

Mathematics Subject Classification ID

Feedback control (93B52) Stabilization of systems by feedback (93D15) Kinematics of a rigid body (70B10) Technical applications of optics and electromagnetic theory (78A55)

Related Items (1)

Magnetometer-only linear attitude estimation for bias momentum pico-satellite

Cites Work

• Fully magnetic attitude control for spacecraft subject to gravity gradient
• Attitude determination and stabilization of a spherically symmetric rigid body in a magnetic field

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