作者: G. Poulin , A. Chemori , N. Marchand
DOI: 10.1080/00207170601069505
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摘要: A global stabilizing control law is proposed for a non-minimum phase under-actuated planar vertical take-off and landing (PVTOL) aircraft. The approach based on receding horizon takes into account the positiveness of thrust its saturation to any arbitrary level. Moreover, angular acceleration can also be bounded. Contrary non-linear optimal control, approach, quadratic programming, improves significantly computational cost algorithm convergence solution insured. chosen function has direct link with energy needed reach desired point which one main worries in design embedded systems such as micro unmanned aerial vehicles (UAV).