交通信息与安全2011，Vol.29Issue(6)：139-142,4.DOI:10.3963/j.ISSN1674-4861.2011.06.032
卡尔曼滤波在飞行器姿态获取系统中的实现
Realization of Kalman Filter in Aircraft Attitude Acquisition System
摘要
Abstract
The hardware design of aircraft attitude control system is introduced. Then, an overall program design and specific hardware selection are given. Moreover, the realization principles and methods of the attitude signal acquisition part are analyzed. The low-pass filter and Kalman filter theory are applied to inhibiting the measurement error of acceleration sensor. The experiment results show that the system can actually determine aircraft's attitude angles of three degrees of freedom, which helps enhance the aircraft's flying qualities.关键词
姿态获取/加速度传感器:卡尔曼滤波/ARMKey words
attitude acquisition/acceleration sensor/Kalman filter/ARM分类
信息技术与安全科学引用本文复制引用
曲春晓,陈伟..卡尔曼滤波在飞行器姿态获取系统中的实现[J].交通信息与安全,2011,29(6):139-142,4.基金项目
武汉理工大学自主创新基金(批准号:2010-ZY-XX-003)资助 （批准号:2010-ZY-XX-003）
