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Satellite cluster flight using on-off cyclic control
DOI:10.1016/j.actaastro.2014.10.004.png)
摘要
En 中文
Nano-satellite clusters and disaggregated satellites are new concepts in the realm of distributed satellite systems, which require complex cluster management mainly regulating the maximal and minimal inter-satellite distances on time scales of years while utilizing simple on-off propulsion systems. The simple actuators and long time scales require judicious astrodynamical modeling coupled with specialized orbit control. This paper offers a satellite cluster orbit control law which works for long time scales in a perturbed environment while utilizing fixed-magnitude thrusters. The main idea is to design a distributed controller which balances the fuel consumption among the satellites, thus mitigating the effect of differential drag perturbations. The underlying methodology utilizes a cyclic control algorithm based on a mean orbital elements feedback. Stability properties of the closed-loop cyclic control system do not adhere to the classical Lyapunov stability theory, so an effort is made to define and implement a suitable stability theory of noncompact equilibria sets. A state selection scheme is proposed for efficiently establishing a low Earth orbit cluster. Several simulations, including a real mission study, and several comparative investigations, are performed to show the strengths of the proposed control law. (C) 2014 IAA. Published by Elsevier Ltd. All rights reserved.
Keyword:
Cluster flight
Cyclic control
On-off thruster
Fuel balance controller
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IF:
3.4
论文数:
1.2W
被引数:
2.1W
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