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Multi-step optimization strategy for fuel-optimal orbital transfer of low-thrust spacecraft

机译:低推力航天器燃料优化轨道转移的多步优化策略

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摘要

An effective method for the design of fuel-optimal transfers in two- and three-body dynamics is presented. The optimal control problem is formulated using calculus of variation and primer vector theory. This leads to a multi-point boundary value problem (MPBVP), characterized by complex inner constraints and a discontinuous thrust profile. The first issue is addressed by embedding the MPBVP in a parametric optimization problem, thus allowing a simplification of the set of transversality constraints. The second problem is solved by representing the discontinuous control function by a smooth function depending on a continuation parameter. The resulting trajectory optimization method can deal with different intermediate conditions, and no a priori knowledge of the control structure is required. Test cases in both the two- and three-body dynamics show the capability of the method in solving complex trajectory design problems
机译:提出了一种在二体和三体动力学中设计燃料最优传递的有效方法。使用变异演算和引物向量理论来制定最优控制问题。这导致了一个多点边界值问题(MPBVP),其特征是复杂的内部约束和不连续的推力曲线。通过将MPBVP嵌入参数优化问题来解决第一个问题,从而简化了一系列横向约束。通过根据连续参数用平滑函数表示不连续控制函数来解决第二个问题。所得到的轨迹优化方法可以处理不同的中间条件,并且不需要先验的控制结构知识。在二体和三体动力学中的测试案例显示了该方法解决复杂轨迹设计问题的能力

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