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

ABASUS里面的边界面模型子程序 -ABASUS inside the bounding surface model subroutine

点云读取，建立包围盒，进行K领域搜索，法向量计算-Point cloud, reading, creating a bounding box, perform the search field K, vector calculation method