针对执行机构受限条件下高超声速飞行器的控制问题,提出一种鲁棒反演控制设计方法.设计一种新的辅助系统对跟踪误差和控制律进行补偿,保证执行器受限时跟踪误差的有界性.为了避免传统反演方法中虚拟导数计算量膨胀问题,引入滑模微分器对虚拟导数进行求解.为了增强系统的鲁棒性,基于改进反正切跟踪微分器(MATD)设计一种新型干扰观测器,对系统的不确定项进行估计和补偿.最后,通过实例仿真验证了所提出控制器的有效性. Aiming at the control problem of hypersonic vehicle with limited actuator, a robust inversion control design method is proposed. A new auxiliary system is designed to compensate the tracking error and the control law to ensure the tracking error Boundedness.In order to avoid the problem of dilation of virtual derivatives in traditional inversion methods, a sliding mode differentiator is introduced to solve the virtual derivatives.In order to enhance the robustness of the system, a modified tangent tracking differentiator (MATD) A new disturbance observer is used to estimate and compensate the uncertainties of the system.Finally, the effectiveness of the proposed controller is verified by an example simulation.