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[source in ebook] PVTOL DL : 0: 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 thrust input to arbitrary saturation limits.
Date : 2025-12-19 Size : 598kb User : 老孙