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.