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首页> 外文期刊>International journal of micro air vehicles >Stochastic Real-Time Optimal Control for Bearing-Only Trajectory Planning
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Stochastic Real-Time Optimal Control for Bearing-Only Trajectory Planning

机译:纯方位轨迹规划的随机实时最优控制

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摘要

A method is presented to simultaneously solve the optimal control problem and the optimal estimation problem for a bearing-only sensor. For bearing-only systems that require a minimum level of certainty in position relative to a source for mission accomplishment, some amount of maneuver is required to measure range. Traditional methods of trajectory optimization and optimal estimation minimize an information metric. This paper proposes constraining the final value of the information states with known time propagation dynamics relative to a given trajectory which allows for attainment of the required level of information with minimal deviation from a general performance index that can be tailored to a specific vehicle. The proposed method does not suffer from compression of the information metric into a scalar, and provides a route that will attain a particular target estimate quality while maneuvering to a desired relative point or set. An algorithm is created to apply the method in real-time, iteratively estimating target position with an Unscented Kalman Filter and updating the trajectory with an efficient pseudospectral method. Methods and tools required for hardware implementation are presented that apply to any real-time optimal control (RTOC) system. The algorithm is validated with both simulation and flight test, autonomously landing a quadrotor on a wire.
机译:提出了一种同时解决纯轴承传感器的最优控制问题和最优估计问题的方法。对于只需要相对于任务完成源在位置上具有最低确定性水平的纯轴承系统,需要一定程度的机动才能测量范围。轨迹优化和最优估计的传统方法使信息度量最小化。本文提出以相对于给定轨迹的已知时间传播动力学来约束信息状态的最终值,这允许以与可针对特定车辆量身定制的一般性能指标的最小偏差实现所需信息水平。所提出的方法不会遭受将信息量度压缩成标量的麻烦,并且提供了一种在操纵到期望的相对点或集合的同时将获得特定目标估计质量的路线。创建了一种算法来实时应用该方法,并使用无味卡尔曼滤波器迭代估计目标位置,并使用有效的伪谱方法更新轨迹。本文介绍了适用于任何实时最佳控制(RTOC)系统的硬件实现所需的方法和工具。该算法已通过仿真和飞行测试验证,使四旋翼自动落在电线上。

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    Commander, 586th Flight Test Squadron, Holloman AFB, NM 88330,Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio 45433;

    Department of Aeronautics and Astronautics,Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio 45433;

    Department of Mathematics and Statistics,Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio 45433;

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