该系统的主要组件，包括一个具有表面空气动力控制的尾段，一个(身体)稳流边条套件，以及组合惯性导引系统和GPS全球定位导引控制基件。
The key components of the system consist of a tail section with aerodynamic control surfaces, a (body) strake kit, and a combined inertial guidance system and GPS guidance control unit.
分析结果可用来研究比例导引系数、系统惯性对脱靶量的影响。
The results can be used to analyse the effect of the proportional navigation coefficient and the inertia of guidance system on miss - distances.
提出了以惯性导航为主、天文导航为辅的一种导航方法，推导出该方法对应的导航基准参数计算模型、导航参数计算模型及天文导航系统的横向导引方程。
A navigation method that the in method is principal and the CN method is subordinate is presented. The calculation model of navigation standard parameter and navigation parameter is deduced.
配备JDAM的炸弹，是由一惯性导引组合系统，耦合到全球定位系统(GPS)接收器来导引，赋予其高达15海里(28公里)公布的范围。
JDAM-equipped bombs are guided by an integrated inertial guidance system coupled to a Global Positioning system (GPS) receiver, giving them a published range of up to 15 nautical miles (28km).
配备JDAM的炸弹，是由一惯性导引组合系统，耦合到全球定位系统(GPS)接收器来导引，赋予其高达15海里(28公里)公布的范围。
JDAM-equipped bombs are guided by an integrated inertial guidance system coupled to a Global Positioning system (GPS) receiver, giving them a published range of up to 15 nautical miles (28km).
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