本文对质量矩控制导弹的动力学方程简化和控制系统的设计进行了研究。详细阐述了所提出的控制方法 ,介绍了径向基单隐层神经网络进行误差补偿的算法原理 ,用Lyapunov理论证明了所采用方法的稳定性。在给出了质量矩导弹的六自由度动力学方程和简化后的方程后 ,用所提出的方法设计控制系统。通过仿真分析 ,得出了本文所提出的方法具有较好的误差补偿能力的结论 In this paper, the research on the simplification of the dynamic equation and the design of the control system of mass moment control missile are studied. The control method proposed in detail is introduced. The algorithm principle of error compensation for radial single hidden layer neural network is introduced. The stability of the proposed method is proved by Lyapunov theory. After giving six-degree-of-freedom kinetic equation and simplified equation of mass moment missile, the control system was designed by the proposed method. Through the simulation analysis, we conclude that the proposed method has better error compensation ability