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Stationkeeping on Unstable Orbits: Generalization to the Elliptic Restricted Three-Body Problem

机译:不稳定轨道上的驻站:椭圆受限三体问题的推广

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摘要

We develop new methods for generating periodic orbits about the collinear libration points and for stabilizing motion on libration orbits using the general formalism of the elliptic restricted three-body problem (ER3BP), Calculation of periodic orbits is accomplished by formulating the ER3BP as a control problem This approach yields halo-like orbits that do not exist without applying active control, having arbitrarily small amplitudes. Linearization about the libration points in pulsating coordinates yields an unstable linear parameter-varying (LPV) system with periodic coefficients. We introduce a continuous acceleration control term into the state-space dynamics and use an LPV-generalized version of the pole-assignment technique to find linear periodic reference trajectories. The nonlinear terms of the equations of motion are then treated as periodic disturbances. A disturbance-accommodating control is used to track the libration-point reference orbit in the presence of nonlinear periodic disturbances. Simulation experiments show that stationkeeping is robust to propulsive dispersions.
机译:我们开发了新的方法来生成绕共线的自由点的周期性轨道,并利用椭圆约束三体问题(ER3BP)的一般形式来稳定自由轨道上的运动。通过将ER3BP表示为控制问题来完成周期性轨道的计算这种方法产生的类晕轨道在没有施加主动控制的情况下是不存在的,具有任意小的振幅。关于脉动坐标中的释放点的线性化会产生具有周期系数的不稳定线性参数变化(LPV)系统。我们将连续加速度控制项引入状态空间动力学中,并使用LPV广义化的极点分配技术来查找线性周期性参考轨迹。然后将运动方程的非线性项视为周期性干扰。在存在非线性周期性扰动的情况下,使用扰动适应控制来跟踪解放点参考轨道。仿真实验表明,驻守对推进弥散具有鲁棒性。

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