Abstract: To protect the aircraft flight safety across the envelope of angle of attack, bifurcation analysis and backstepping method are investigated to predict and suppress the unstable nonlinear flight phenomena. By applying ...

Abstract: To achieve tracking performance and robustness simultaneously during an aircraft’s autonomous short landing phase, a three-dimensional automatic landing system designed using robust adaptive backstepping control is ...

Abstract: A new extended lattice model of traffic flow is presented by taking into account both multianticipative behavior and the reactiontime delay of drivers. The linear stability theory and the nonlinear analysis method are ...