AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
Online ISSN : 1884-0477
ISSN-L : 1884-0477
Development of the Attitude Sensing System using Thermopile Sensors
Masayuki KURIBARAToshiki MOCHIZUKIHiroshi TOKUTAKE
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2015 Volume 14 Pages 7-15

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Abstract
An attitude sensing system using thermopile sensors and inertial sensors was proposed. The output model of the thermopile sensor was constructed from the calibration experiment and the theoretical calculations. The estimation algorithm of the attitude angles was developed from the sensor output models using extended Kalman filter. Because thermopile sensor output correlates with attitude to the ground directly, the error of inertial sensors can be compensated. Additionally, the proposed system consists of commercial low-cost product. Numerical simulations and experiment were carried out and the performance was validated. Experimental result shows that the proposed system has precision of approximately 1.2°.
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© 2015 The Japan Society for Aeronautical and Space Sciences
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