作者: I. Fantoni , A. Zavala , R. Lozano
关键词: Bounded function 、 Thrust 、 Saturation (chemistry) 、 Takeoff and landing 、 Nonlinear system 、 Control theory 、 Planar 、 Engineering 、 Bounding overwatch 、 Aerospace engineering
摘要: A global stabilizing control design is proposed for the planar vertical takeoff and landing (PVTOL) aircraft. The methodology based on use of nonlinear combinations saturation functions bounding thrust input to arbitrary limits. algorithm simple provides convergence state origin.