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A CONTROL ALGORITHM FRAMEWORK FOR TIME-OF-ARRIVAL AND ARRIVAL AIRSPEED CONTROL

机译:到达时间和到达空速控制的控制算法框架

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This paper documents the framework for a control algorithm which commands an aircraft to arrive at a specified final location with constraints on arrival time, airspeed, and heading in an environment with steady state wind and turbulence. The path is defined as a variable-length racetrack, allowing for an accurate estimate of the arrival time which can be quickly changed by increasing or decreasing the size of the racetrack. The arrival time is estimated using Gaussian quadrature which allows for the inclusion of steady state wind into the arrival time estimate. The time-of-arrival error between the estimated and the desired arrival time is then minimized through real-time path and airspeed control. A sensitivity study was performed which varied aircraft performance, wind speed, wind direction, arrival time and magnitude of turbulence. The results show the controller achieved a time-of-arrival error of less than one second and arrival airspeed error less than four meters per second across all simulations with moderate turbulence and wind speed less than one third the desired airspeed of the vehicle.
机译:本文介绍了一种控制算法的框架,该控制算法命令飞机在抵达时间,空速和在具有稳定状态风和湍流的环境中进行约束的指定最终位置。该路径被定义为可变长度的赛道,允许通过增加或减少赛道的大小可以快速改变到达时间的准确估计。使用高斯正交估计到达时间,允许将稳态风纳入到达时间估计中。然后通过实时路径和空速控制最小化估计和期望的到达时间之间的到达时间误差。进行了敏感性研究,多种飞机性能,风速,风向,到达时间和湍流幅度。结果表明,控制器在所有模拟中达到小于4米的到达时间误差小于一秒,并且在所有模拟中,湍流和风速小于车辆的所需空速速度小于4米。

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