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讨论了空空导弹捷联惯导系统传递对准中主惯导系统导航参数的应用问题,讨论了在火控系统中建立惯性基准系的原理和计算方法,指出了采用惯性基准系在空空导弹传递对准中的优缺点。
This paper discusses the application of the navigation parameters of the main navigation system of the airborne missile strapdown inertial navigation system, and discusses the principle and calculation method of establishing the inertial reference system in the fire control system. It is pointed out that the inertial reference system is used in air-to-air missile transmission The pros and cons of alignment.