本文论述了根据发射区评价导弹性能的方法,分析了妨碍导弹正常飞行的因素;导弹的姿态变化、攻角及负载系数等。同时还探讨了制导方式和发射的初始条件等,并通过模拟证明了缓和这些限制就可以提高命中精度。 This paper discusses the method of evaluating the missile performance based on the launching area, analyzes the factors that hinder the normal flight of the missile, the attitude change of the missile, the angle of attack and the load factor. At the same time, the guidance methods and the initial conditions of launching are also discussed. Simulations have shown that the mitigation of these restrictions can improve the accuracy of hits.