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Box Particle Control for Aerospace Vehicles Guidance Under Failure Probability Constraints

机译:失效概率约束下航空航天器制导的盒粒子控制

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Determining a constrained optimal trajectory remains tricky when the state suffers non-analytical uncertainty and when the feasible set is non-convex. This paper presents a chance constrained trajectory planning approach, called Box Particle Control (BPC), which guarantees an a priori specified maximum probability of constraints violation along a predicted trajectory. This failure probability is estimated by approximating the state density with a mixture of bounded kernels, defined by weighted box particles, and is used as a constraint in an optimization scheme. Numerical simulations illustrate the performance of BPC, which ensures the constraints satisfaction even for low numbers of box particles. The BPC makes it possible to tackle non-analytic state densities (e.g., multimodalities) and non-convex feasible sets with a higher robustness and a 60% lower computational load than previous approaches in terms of number of elementary operations.
机译:当状态遭受非分析不确定性且可行集非凸时,确定约束的最佳轨迹仍然很棘手。本文提出了一种机会受限的轨迹规划方法,称为盒粒子控制(Box PC,BPC),该方法可确保沿预测轨迹事先指定的最大违规约束概率。该故障概率是通过用加权盒子粒子定义的有界内核的混合近似状态密度来估计的,并在优化方案中用作约束。数值模拟说明了BPC的性能,即使对于少量的盒子颗粒,它也可以确保约束满足。与基本方法相比,BPC能够以比以前的方法更高的鲁棒性和60%的计算量来解决非分析状态密度(例如,多模态)和非凸可行集。

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