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首先分析了加速度计组合测量载体线加速度和角速度的原理。进而讨论了针对火箭炮或身管火炮的捷联惯性导航原理。最后给出了无陀螺捷联惯性导航系统的框图
Firstly, the principle of accelerometer to measure the linear acceleration and angular velocity of the carrier is analyzed. Then discussed the principle of strapdown inertial navigation for rocket launchers and barrel guns. Finally, a block diagram of gyro-free strapdown inertial navigation system is given