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Academy transaction note ?closed form solution for a minimum deviation magnetically controllable satellite angular trajectory?
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DOI：10.1016/j.actaastro.2022.11.045.png)
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摘要
En 中文
Purely magnetic satellite attitude control is considered. Special reference motion is constructed which provides local controllability. The angular trajectory is found in the neighborhood of unstable gravity gradient torque equilibrium. Direct solution for the minimization of the quadratic cost function representing the deviation from the equilibrium is derived. Linear equality type constraint on the torque direction is imposed. This solution is compared to the one found by the particle swarm optimization.
Keyword:
Three-axis magnetic control
Attitude control
Particle swarm optimization
Reference motion
Pseudo inverse matrix
期刊
IF:
3.4
论文数:
1.2W
被引数:
2.1W
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引用论文
Asymptotic study of a complete magnetic attitude control cycle providing a single-axis orientation.png)
ACTA ASTRONAUTICA
ACTA ASTRONAUTICAIF3.4
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