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In the process of reentry trajectory optimization of glide hypersonic vehicle, a new adaptive detection point pseudospectral method based on detection point is proposed to solve the problem of no-fly zone constraints between adjacent collocation points. This method adaptively adjusted the number of discrete subintervals and the number of collocation points in the interval according to the maximum...
Based on the LQR optimal control, a method for the BTT control of cruise missile was proposed. The mathematical model of the cruise missile based on the aerodynamic externality and aero characteristic was established. Then choose the appropriate state variable follow the design request of the control. Design the optimal control law based on the integral LQR. The simulation results show that the missile...
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