反导导弹垂直发射初段控制设计初探

以国外某先进反导导弹为研究对象，探讨了反导导弹在空气动力舵快速响应及较高出速速度条件下，快速准确地完成初始段转弯，瞄准任务的垂直发射技术的理论与工程方法，提出了一种基于轨道控制力理论的反导导弹垂直发射初段控制最优化方法及一种在工程上较为实用的导弹飞行冲角变化函数，此外，还提出了一种跨音速S状程序转弯飞行的新方法。

Control Design Research on Initial Guidance Phase of Vertical Launching Anti-Missile Missile

This paper that bases on one type of foreign advanced anti missile missile whose atmosphere dynamical helm responds quickly and initial velocity is high, is in order to study the academic and engineering method of a vertical launching anti missile missile which must be turn and aim quickly in its initial guidance phase. In this paper, an optimization method based on orbit control force is produced. A function of flight program angle transformation which can be used in a practical project is introduced. A new way which can make the missile turn stably liking 'S' in the transonic region is also introduced.