Description: 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. Platform: |
Size: 612352 |
Author:老孙 |
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