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Three-Dimensional Trajectory Optimization Design of Parafoil System Obstacle Avoidance Based on Switched System Method

机译:基于切换系统方法的翼型系统避障三维轨迹优化设计

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We research on a problem for three-dimensional trajectory optimization design of parafoil systems obstacle avoidance. Since open-loop control lacks of robustness in practical engineering applications, to ensure the robustness of system, by devising a new piecewise state feedback controller, we convert previous problem to the closed-loop switched systems optimal control problem with state inequality restrictions. Due to the unknown switching instants and the existence of such restrictions, we have difficulty in handling this problem by employing classical optimization methods. To address faced dilemma, time-scaling transformation and smoothed penalty approach are applied. Finally, an unconstrained parameter optimization problem is derived, and an improved conjugate gradient algorithm is introduced for addressing this problem. Simulation experiment indicates proposed algorithm is valid, and a desired three-dimensional trajectory of parafoil is obtained and avoids terrain obstacles to reach the landing point more precisely.
机译:我们研究了翼型系统避障的三维轨迹优化设计问题。由于开环控制在实际工程应用中缺乏鲁棒性,为了确保系统的鲁棒性,通过设计新的分段状态反馈控制器,我们将先前的问题转换为具有状态不等式约束的闭环切换系统最优控制问题。由于未知的切换时刻和此类限制的存在,我们很难通过采用经典的优化方法来解决此问题。为了解决面临的困境,应用了时标变换和平滑惩罚方法。最后,推导了无约束参数优化问题,并提出了一种改进的共轭梯度算法来解决该问题。仿真实验表明,该算法是有效的,并获得了理想的三维翼型轨迹,避免了地形障碍物更精确地到达着陆点。

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