B.R. Andrievsky and A.L. Fradkov (Russia)
Adaptive control, Identification, Sliding mode controller, UAV Guidance
Combined adaptive control law for an autopilot of the UAV homing guidance system is proposed. The adaptation al gorithm provides prescribed attitude motion dynamics for different flight conditions. Simulation results verify effi ciency of the combined adaptive controller in the case of significant uncertainty of the UAV parameters and time dependence of the guidance loop.
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