Analysis of formation flying control of a pair of nano-satellites

S. Veres, Stephen B. Gabriel, E. Rogers, D. Mayne
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引用次数: 23

Abstract

Gives an analysis and provides implementable solutions for constrained control problems of stabilization and maneuver control of two nano-satellites. The methodology provides solutions under various constraints of propulsion and differential drag control: magnitude constraints, disturbances and measurement errors are taken into account. The methods are illustrated in simulation of a realistic nano-satellite pair.
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一对纳米卫星编队飞行控制分析
对两颗纳米卫星的稳定和机动控制约束问题进行了分析,并给出了可行的解决方案。该方法提供了在推进和微分阻力控制的各种约束下的解:考虑了量级约束、干扰和测量误差。最后以实际的纳米卫星对为例进行了仿真。
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