For the existence of model uncertainties and complex environment such as pneumatic robust control problem in the aircraft terminal guidance process, introduce a control scheme based on the optimal ratio of three-dimensional ADRC sliding mode guidance law. The online dynamic feedback controller can compensate for the impact of external interference to enhance the robustness of the system, the simulation results show that the scheme has higher guidance precision and strong robustness.
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吕永佳. 基于自抗扰三维最优比例滑模导引律设计[J]. 科学技术与工程, 2011, (12): . lvyongjia. Design of the three-dimensional optimal ratio sliding mode guidance law based on auto-disturbance rejection (ADRC)[J]. Science Technology and Engineering,2011,(12).