Control method of hypersonic vehicle orienting uncertainty condition
A technology of hypersonic speed and control method, applied in attitude control, three-dimensional position/course control, etc., can solve problems such as slow convergence speed and chattering, and achieve the effect of ensuring rapidity and robustness
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[0138] In order to verify the control effect of the designed backstepping sliding mode controller, the hypersonic vehicle is simulated and analyzed, the command tracking signal is given, and the parameters of the designed controller are adjusted at the same time to obtain the corresponding command tracking effect. The robustness of the control method is verified by introducing the maximum parameter perturbation into the aircraft model, which shows that the control method greatly improves the stability and accuracy of the system.
[0139] The following is a simulation verification of the established hypersonic aircraft model from the perspective of simulation. In the Matlab simulation test, refer to the simulation verification conditions in the document "Backstepping Sliding Mode Control for Hypersonic Vehicle Trajectory Tracking" to select the flight height and flight speed of the aircraft The initial equilibrium states of are respectively the nominal parameters under the 33528...
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