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Hybrid Genetic Algorithm Collocation Method for Trajectory Optimization

机译:混合遗传算法的轨迹优化配置方法

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RESEARCH of recent decades has uncovered many advances innthe development of numerical trajectory optimization. Thesenmethods are attempts to solve discretized versions of some form of annoptimal control problem that, in general, cannot be solved analyticallynusing Pontryagin’s minimum principle [1]. Numerousntechniques exist, each one parameterizing the problem and enforcingnthe equations of motion differently. One such technique is that ofndifferential inclusions, which constrains the discretized states atnadjacent nodes to lie on the attainable sets given the admissiblencontrol inputs [2]. Alternatively, direct shooting methods discretizenthe control history and integrate the equations of motion to obtain thenstate histories and evaluate the constraint violations [3]. A thirdntechnique, collocation, enforces the equations of motion throughnconstraints on the derivative of an interpolating function and the statenequations [4]. These various methods have been applied to a numbernof problems, including space vehicle reentry trajectories [5],nkinematic path planning for unmanned aerial and ground vehiclesn[6], spacecraft slewing maneuvers [7,8], and low-thrust orbitntransfers [9–12].
机译:近几十年来的研究发现了数值轨迹优化发展的许多进展。感觉方法是尝试解决某种形式的非最优控制问题的离散形式,这些问题通常不能用庞特里亚金的最小原理来解析地解决[1]。存在许多技术,每个技术都对问题进行参数化并以不同方式执行运动方程。一种这样的技术是微分包含,它在给定的控制输入允许的情况下,将不相邻节点的离散状态约束在可达到的集合上[2]。另外,直接射击方法可以离散化控制历史并整合运动方程,从而获得状态历史并评估约束违规[3]。第三种技术,搭配,通过对插值函数的导数和状态方程的约束来强制运动方程[4]。这些不同的方法已应用于许多问题,包括航天器的再入轨迹[5],无人驾驶的飞机和地面飞行器的运动路径规划[6],航天器的回旋操纵[7,8]和低推力轨道转移[9– 12]。

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