摘要: In order to solve the problems of time and angle control of the missile, such as the lack of information, and limited application conditions, an internal angle guidance law based on geometric relationship is proposed, with which t... 展开 In order to solve the problems of time and angle control of the missile, such as the lack of information, and limited application conditions, an internal angle guidance law based on geometric relationship is proposed, with which the control point is calculated by successive approximation. Supported by the guidance law, a feedforward and feedback compound guidance control scheme on the basis of the virtual target is designed. The simulation results have shown that the convergence speed is faster, the accuracy of time and angle control is much higher, and the calculation amount successfully meets the real-time requirements. 收起