飞航导弹大空域机动弹道的最优设计

在飞航导弹飞行经过的空域内设置好若干个导航点，利用最优控制方法引导导弹依次通过这些导航点，实现了控制能量最优的机动飞行弹道。推导了基于捷联惯导控制方案的导弹最优控制过载指令公式，并进行了仿禀验证。仿真结果表明，该方案提高了导弹的突防性能，具有较好的应用价值。

Optimal Design of Mobile Trajectory in Large Space for Aerodynamic Missile

Setting several navigation points in airspace which missile will fly through, leading the missile to go through these points in turn by the way of optimal control, so the mobile trajectory whose control energy is optimal can be realized. The formulae of optimal control overload commands are reckoned. Finally the simulation results prove that the missile's maneuverability is greatly improved and the control scheme has preferable theoretical and practical worth.