本文研究的就是一种用于炮射导弹的新型发射技术，即应用高低压发射原理的二次发射技术。
This dissertation focuses on the study of a new launching technology of missile by the gun, in which the high-low launching theory is applied to the two-stage propulsion technology.
针对某单通道控制炮射导弹所采用的自激振荡线性化舵机，给出了一种有效的舵机延迟补偿时间处理方法。
An effective method was proposed to deal with delay compensation time of self-oscillation linear actuator for a gun launched missile controlled with single channel.
文中根据炮射导弹的射击特点，分析了炮射导弹落点精度的概念及其相关指标，提出了评定炮射导弹落点精度的方法。
Based on the fire characteristic of gun-launched missile, both the concept of the impact accuracy and the relevant index of gun-launched missile were analyzed, the assessment method was also proposed.
文中根据炮射导弹的射击特点，分析了炮射导弹落点精度的概念及其相关指标，提出了评定炮射导弹落点精度的方法。
Based on the fire characteristic of gun-launched missile, both the concept of the impact accuracy and the relevant index of gun-launched missile were analyzed, the assessment method was also proposed.
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