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This paper proposes a novel integrated guidance and autopilot (IGA) method for hypersonic vehicles in dive phase. The third order back-stepping L1 adaptive control is implemented to deal with the uncertainties of aerodynamics coefficients, degradation of control surface efficiency and unmatched time-varying disturbances in the nonlinear flight dynamics. Furthermore, a second order actuator dynamics...
This paper proposes a novel method for the integrated guidance and control (IGC) of glider in dive and pull-up trajectory. The main objective is robust and adaptive tracking for flight path angle (FPA). Firstly, the integrated guidance and autopilot nonlinear model is built based on the IGC with a second order rudder dynamics. Then the back-stepping Ii adaptive control is implemented to deal with...
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