助推-滑翔导弹弹道优化研究

A Study of Optimal Trajectory for Boost-glide Missile

针对助推-滑翔导弹的弹道优化问题,给出了一种求解其最大射程弹道的分段优化方法,建立了其纵平面运动模型和弹道优化模型。在考虑攻角绝对值、攻角变化率、法向过载、分离点攻角衔接及落地条件等约束下,应用序列二次规划法求解了其最大射程弹道。分析表明,助推-滑翔导弹比传统弹道导弹射程显著提高,其最优弹道的起伏有助于增大射程和提高突防能力。

Boost-glide missile is associated with a kind of unique trajectory.A method that boost phase and glide phase were optimized separately,was proposed which optimized the range of boost-glide missile.The equations of motion and optimization model for the boost-glide trajectory were presented.The sequential quadratic programming algorithm was used to solved the optimization problem.The maximum range of the boost-glide missile with the constraints of change rate and absolute value for angle-of-attack,the constra...