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Multi-Objective Optimal Control of Ascent Trajectories for Launch Vehicles

机译:运载火箭上升轨迹的多目标最优控制

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This paper presents a novel approach to the solution of multi-objective optimal control problems. The proposed solution strategy is based on the integration of the Direct Finite Elements Transcription method, to transcribe dynamics and objectives, with a memetic strategy called Multi Agent Collaborative Search (MACS). The original multi-objective optimal control problem is reformulated as a bi-level nonlinear programming problem. In the outer level, handled by MACS, trial control vectors are generated and passed to the inner level, which enforces the solution feasibility. Solutions are then returned to the outer level to evaluate the feasibility of the corresponding objective functions, adding a penalty value in the case of infeasibility. An optional single level refinement is added to improve the ability of the scheme to converge to the Pareto front. The capabilities of the proposed approach will be demonstrated on the multi-objective optimisation of ascent trajectories of launch vehicles.
机译:本文提出了一种解决多目标最优控制问题的新颖方法。提出的解决方案策略基于直接有限元转录方法的集成,以记录动态和目标,并采用了一种称为“多主体协作搜索(MACS)”的模因策略。将原始的多目标最优控制问题重新表述为双层非线性规划问题。在外部级别(由MACS处理),将生成试验控制向量并将其传递到内部级别,从而增强了解决方案的可行性。然后将解决方案返回到外部层次,以评估相应目标函数的可行性,并在不可行的情况下增加惩罚值。添加了可选的单级优化,以提高该方案收敛到Pareto前沿的能力。拟议方法的能力将在运载火箭上升轨迹的多目标优化中得到证明。

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