NDLI: Application of MIMU/magnetometer integrated system on the attitude determination of micro satellite

Content Provider	IEEE Xplore Digital Library
Author	Su, K. Ren, D.H. You, Z. Zhou, Q.
Copyright Year	2004
Abstract	Micro Inertial Measurement Unit (MIMU) has given Inertial Measurement Unit (IMU) a widely application respective. In this paper, we study the application of MIMUl magnetometer integrated system on the attitude determination of micro satellite. Based on the principle of MIMU and the` measurement of magnetometer, MIMU/magnetometer system is integrated. Through designing the simulatien models of attitude determination for micro satellite, consisted of< the `SGP4 orbit model, the IGRF model and the satellite dynamic model, we do the simulation research. Simulation results with EKF show that, in 1/3 orbit time, the measurement error of attitude angular is controlled within 0.5 deg, meeting the requirement of the micro satellite attitude determination. In addition, we compare the UKF results with the EKF and find the UKF results converge faster than the EKF while the state estimate precision of the two filters are comparable.
Starting Page	579
Ending Page	583
File Size	372395
Page Count	5
File Format	PDF
ISBN	0780387481
DOI	10.1109/ICIMA.2004.1384262
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2004-08-26
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Magnetometers Position measurement Satellites Extraterrestrial measurements Magnetic field measurement Measurement units Earth Geomagnetism Coordinate measuring machines Measurement errors
Content Type	Text
Resource Type	Article

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4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
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