A New Control Scheme for Satellite Formation Reconfiguration

A New Control Scheme for Satellite Formation Reconfiguration
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一种新的卫星编队重构控制方案

DOI:
10.2322/tjsass.53.258
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发表时间:
2011-02
影响因子:
1.1
通讯作者:
Wang, Feng
Wang, Feng
中科院分区:
工程技术4区
文献类型:
--
作者:
Wang, Jihe;Zhang, Jinxiu;Cao, Xibin;Wang, Feng

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在假设编队中成员星序列不变的情况下,提出了一种新的控制方案,利用脉冲控制将编队的构形从一条椭圆相对轨道(车轮轨道)改变到另一条椭圆相对轨道。首先,分别推导了脉冲机动平面内和平面外变轨问题的燃料最优解。其次,利用这些燃料最优脉冲控制策略解决了单星轨道重构问题。基于燃料最优的单星重构解,提出了一种新的卫星编队重构异步控制方案。该控制方案能够实现编队总燃料消耗最小、单星燃料消耗均衡和编队卫星间避免碰撞的目标。此外,这种新的控制方案具有解析形式,便于星上应用。这种新的控制方案的局限性是,随着成员卫星的增加,总的重构时间成比例地增加。
Assuming that the sequence of the member satellites in a formation is unchanged, this paper presents a new control scheme to change the configuration of the formation from one elliptic relative trajectory (cart-wheel orbit) to another elliptic relative trajectory by using impulsive control. First, the full analytical fuel-optimal solutions of in-plane and out-of-plane orbit transfer problems using impulsive maneuver are derived, respectively. Next, the single satellite orbit reconfiguration problem is solved by using these fuel-optimal impulsive control strategies. Based on the fuel-optimal single satellite reconfiguration solutions, a new asynchronous control scheme for satellite formation reconfiguration is proposed. This new control scheme can achieve the objectives of total minimum fuel consumption of the formation, balanced fuel expenditure of the single satellite, and collision avoidance between the satellites in formation. Furthermore, this new control scheme has an analytical form, so it is simple and convenient for onboard application. The limitation of this new control scheme is that as the member satellites increases, the total reconfiguration time increases proportionally.
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