Research on a New Eight-Accelerometer Configuration for Attitude Angle Calculation of UAV

摘要：

The scheme to calculate attitude angle of UAV was introduced to replace high-priced angular velocity gyroscope, so as to lower the cost of UAV. A new eight-accelerometer configuration for attitude angle calculation of UAV was proposed. It can optimize algorithm, remove accumulative error in process of calculation and improve calculation precision through multi-sensor redundant information. The digital simulation results show that attitude angle calculation can satisfy current requirements and has low calculation error and time accumulation, which is of practical significance to research on inertia device.

关键词： UAV attitude angle calculation accelerometer

作者: SONG Lei HUANG Chang-qiang WENG Xing-wei WU Wen-chao

作者单位: Engineering College, Air Force Engineering University, Xi’an 710038, China

会议类型: 国际会议

会议名称: The 22nd China Control and Decision Conference(2010年中国控制与决策会议)

会议地点: 徐州

会议语种:英文

页码: 4119-4123

在线出版日期: 2010-05-26（万方平台首次上网日期，不代表论文的发表时间）