固定翼
模型预测控制
控制理论(社会学)
路径(计算)
计算机科学
控制(管理)
翼
航空航天工程
工程类
人工智能
计算机网络
作者
Ahmed S. Rezk,Horacio M. Calderón,Herbert Werner,B. Herrmann,Frank Thielecke
摘要
This paper presents a cascaded approach for a predictive path-following scheme using quasi-linear parameter-varying model predictive control (qLMPC) applied to a 25 kg unmanned aerobatic aircraft. The quasi-linear parameter-varying (qLPV) representation provides a semi-linear model of the nonlinear system, while fast solvers are utilized to solve quadratic optimization problems (QOPs) in milliseconds. To incorporate integral action and overcome wind disturbances, a velocity-based linearization of the model is employed. Two scenarios with nine waypoints each are evaluated using a hybrid strategy that combines arc-length parameterization with cubic splines and a synthetic waypoint path-planner. The path-following strategy is applied to both simplified kinematic and high-fidelity models of the aircraft, with constant wind in the first scenario and time-varying wind in the second scenario. The algorithm achieves good performance in both scenarios with short computation times. Lastly, a performance analysis of the strategy with the two path-planning techniques is presented.
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