采用Nussbaum增益滑模自适应控制方法解决导弹制导控制一体化设计问题.充分考虑一体化模型具有通道间耦合、气动建模不确定性、气动参数摄动和目标机动引起的干扰等特点,基于自适应控制对未知量的辨识能力和滑模控制的抗干扰能力,以及Nussbaum增益控制对系数不确定系统所具有的较好的控制能力,设计Nussbaum增益滑模自适应控制律,并证明系统的稳定性.仿真结果验证了所提出方法的有效性. The Nussbaum gain sliding mode adaptive control method is used to solve the integrated design of missile guidance control system. Considering that the integrated model has the characteristics of interchannel coupling, aerodynamic modeling uncertainty, aerodynamic parameter perturbation and disturbance caused by target maneuver, Adaptive control of the unknowns’ identification ability and anti-jamming capability of sliding mode control, and the Nussbaum gain control has better control ability to the system with uncertain coefficients, the Nussbaum gain sliding mode adaptive control law is designed, and the stability of the system is proved The simulation results verify the effectiveness of the proposed method.