修正弹道的飞行稳定性研究

弹道修正弹是减小弹道散布的一个新弹种，文中讨论了在不同修正力作用下，对弹丸绕心动力攻角方程中诸非齐次项对应特解的影响情况，推导了这些影响的关系式，分析了影响程度与可能出现的状况，对今后深入开展有关该弹种的研究工作，有一定参考意义。

THE RESEARCH OF FLIGHT STABILITY FOR A PROJECTILE WITH CORRECTED TRAJECTORY

The projectile, which trajectory could be simply corrected during flight in order to improve its dispersion, is a new kind of projectiles. The correcting forces will affect the special solutions of angle of attack. The paper discusses the influence and sets up some formula of angles to the flight stabilities of the projectile. The results are very useful to research detailed performance for this kind of projectiles in future.