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Autonomous space systems control incorporating automated maneuvers strategies in the presence of parameters uncertainties

机译:在参数不确定的情况下,结合了自动操纵策略的自主空间系统控制

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The research attempts to deal with the autonomous space systems incorporating new automated maneuvers strategies in the presence of parameters uncertainties. The main subject behind the investigation is to realize the high-resolution small amplitude orbital maneuvers via the first control strategy. And subsequently to realize the large amplitude orbital maneuvers via the second control strategy, as well. There is a trajectory optimization to provide the three-axis referenced commends for the aforementioned over actuated autonomous space system to be able to transfer from the initial orbit to its final ones, in finite burn, as long as the uncertainties of key parameters of the system such as the thrust vector, the center of the gravity, the moments of the inertia and so on are taken into real consideration. The strategies performances are finally considered through a series of experiments and a number of benchmarks to be tangibly Verified. (C) 2016 ISA. Published by Elsevier Ltd. All rights reserved.
机译:该研究试图在参数不确定性存在的情况下处理结合了新的自动化机动策略的自主空间系统。研究的主要课题是通过第一种控制策略实现高分辨率的小振幅轨道机动。随后也通过第二种控制策略来实现大振幅轨道机动。有一种轨迹优化方法,可以为上述过驱动的自主空间系统提供三轴参考称赞,以便能够在有限燃烧中从初始轨道转换到最终轨道,只要系统关键参数的不确定性即可诸如推力矢量,重心,惯性矩等都被真正考虑在内。最后,将通过一系列实验和一些基准对战略绩效进行评估,以进行切实验证。 (C)2016 ISA。由Elsevier Ltd.出版。保留所有权利。

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