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Calibration of Inertial Measurement Units Using Pendulum Motion
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  • Calibration of Inertial Measurement Units Using Pendulum Motion
  • Calibration of Inertial Measurement Units Using Pendulum Motion
저자명
Choi. Kee-Young,Jang. Se-Ah,Kim. Yong-Ho
간행물명
International journal of aeronautical and space sciences
권/호정보
2010년|11권 3호|pp.234-239 (6 pages)
발행정보
한국항공우주학회
파일정보
정기간행물|ENG|
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기타
이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
서지반출

기타언어초록

The utilization of micro-electro-mechanical system (MEMS) gyros and accelerometers in low-level inertial measurement unit (IMU) influences cost effectiveness in a positive way under the condition that device error characteristics are fully calibrated. The conventional calibration process utilizes a rate table; however, this paper proposes a new method for achieving reference calibration data from the natural motion of pendulum to which the IMU undergoing calibration is attached. This concept was validated with experimental data. The pendulum angle measurements correlate extremely well with the solutions acquired from the pendulum equation of motion. The calibration data were computed using the regression method. The whole process was validated by comparing the measurement from the 6 sensor components with the measurements reconstructed using the identified calibration data.