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研究了一种中远程战术导弹的捷联复合制导系统最优末制导指令的设计．重点研究了增加速率陀螺和加速度计反馈时对系统的影响．基于最优控制理论的二次型性能指标，将弹体-自动驾驶仪惯性设计为三阶受控对象，导出了最优制导指令的解析表达式．数字仿真结果表明，所作分析与设计是有效的。
The design of the optimal terminal guidance for a SINS guided missile system is studied. Focus on the rate gyro and accelerometer feedback on the system. Based on the quadratic performance index of optimal control theory, the inertia of projectile-autopilot is designed as the third-order controlled object, and the analytical expression of optimal guidance order is derived. The numerical simulation results show that the analysis and design are effective.