对某型垂直起降飞机在推力有界限制条件下进行三种情况下的仿真研究-Global stabilizing control design is proposed for the planar vertical takeoff and landing (PVTOL) aircraft. The methodology is based on the use of nonlinear combinations of saturation functions bounding the thrus

抗积分饱和PID控制算法及仿真，含有积分饱和的算法代码(Anti - integral Saturation PID Control Algorithm and Simulation)