针对微下击暴流风切变会对飞行器造成严重危害的情况,分析了微下击暴流风切变的成因和Vicroy数学模型,为了使飞机有效避开微下击暴流风切变危险区,结合空气动力学和飞行力学,提出了飞行控制算法,并与传统的控制算法进行了对比分析;仿真结果表明,提出的控制算法能较好地实现路径控制,并优于传统的PID和s0FNN控制算法。
The microburst wind shear can be dangerous to aircraft, particularly causing fatal crash. In this paper, the cause of microburst wind shear and Vicroy mathematical model are analyzed and a new flight control algorithm is proposed by combining aerodynamics and flight mechanics to avoid the danger area of the microburst wind shear. The simulation results show that the proposed control algorithm can achieve a better path control than better than the traditional PID and SOFNN control algorithm.