Optimal Balanced-Energy Formation Flying Maneuvers
Optimal Balanced-Energy Formation Flying Maneuvers
复制标题
最佳平衡能量编队飞行动作
DOI：
10.2514/1.19199
复制
发表时间：
2006
影响因子：
2.6
通讯作者：
F. Hadaegh
中科院分区：
文献类型：
--
作者：
A. Rahmani;M. Mesbahi;F. Hadaegh
航天器编队飞行最近在空间系统界被提出和研究，作为一种有希望的替代单片和经常是大型空间结构的方法。这种分布式空间系统的最佳平衡能量控制有可能延长其使用寿命，并可作为任务可行性研究的重要基线。本文提出了一种二、三航天器分布式空间系统的最优能量平衡控制策略。在此过程中，我们将描述在深空以及在地球引力影响范围内操作的相关任务场景。仿真结果表明，我们的理论分析的后果也提供。
Spacecraft formation flying has recently been proposed and examined in the space systems community as a promising alternative to monolithic and often large space structures. Optimal balanced-energy control of such distributed space systems potentially increases their lifetime and can serve as an important baseline in mission feasibility studies. In this paper, an optimal balanced-energy control strategy for two- and three- spacecraft distributed space systems is proposed. Along the way, we will delineate relevant mission scenarios in deep space, as well as those that operate in Earth's gravitational sphere of influence. Simulation results demonstrating the ramifications of our theoretical analysis are also provided.