Abstract : A method to realize attitude algorithm module in strapdowninertialguidance is presented.
摘要 ： 提出了捷联惯性导航系统姿态解算模块的一种实现方法。
2
The paper introduces a very low cost strapdowninertialguidance system consisting of piezoelectric gyros and low cost accelerometers.
提出一种低成本捷联惯性制导系统方案。该系统主要由压电陀螺和低成本加速度计构成。
3
A mini digital Attitude and Heading Reference System (AHRS) based on DSP is designed, which can be used on air-to-air missile with StrapdownInertial Navigation System (SINS) as mid-course guidance.