Analysis of formation flying control of a pair of nano-satellites
Analysis of formation flying control of a pair of nano-satellites
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一对纳米卫星编队飞行控制分析
DOI：
10.1109/cdc.2001.981031
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发表时间：
2001
期刊：
影响因子：
--
通讯作者：
D. Mayne
中科院分区：
文献类型：
--
作者：
S. Veres;Stephen B. Gabriel;E. Rogers;D. Mayne
对两颗纳米卫星稳定与机动控制的约束控制问题进行了分析并提供了可实施的解决方案。该方法提供了各种推进和差动阻力控制约束下的解决方案：考虑了幅度约束、干扰和测量误差。这些方法通过对现实纳米卫星对的模拟进行说明。
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.