摘要
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。
Firstly, a method using linear accelerometers to measure the linear acceleration and angular velocity of a vehicle is presented.Secondly, the principle of strap down inertial navigation for a rocket or cannon artillery is analyzed in details. Finally, the block diagram of the strap down inertial navigation system is given .
出处
《探测与控制学报》
CSCD
1999年第4期3-6,共4页
Journal of Detection & Control
关键词
无陀螺
捷联
惯性导航
弹道修正
引信
nongyroscope
strap down
inertial navigation
trajectory correcting fuze
