摘要
针对目前捷联式姿态航向系统低成本、低功耗、高精度、微型化的发展趋势,提出一种基于MEMS器件的姿态航向系统的实现方案,介绍了该系统的方案设计与算法原理,实验证明该系统可以很好的测量出载体的姿态航向,可用于小型无人直升机的导航控制中。
In view of the current strapdown attitude and heading system's development trend in low cost, low power, high accuracy and miniaturization, an implementation of attitude and heading system based on MEMS devices is proposed. The system's design and algorithm theory are introduced. The experiment proves that the system can get a good result on measuring attitude,which can be embedded in navigation of small unmanned helicopter control.
出处
《电脑知识与技术》
2009年第11X期9527-9529,9533,共4页
Computer Knowledge and Technology
