Research on the high accuracy rapid test method of IMU

Yuhang Xuebao/Journal of Astronautics

Volumn 29, Issue 1, 2008, Pages 172-177

  Xiao, Long Xu ^a   Wei, Shi Hui ^a   Sun, Wen Sheng ^b  

^a The Second Artillery Equipment Academe   (China)

^b The Second Artillery Military Commissary   (China)

Author keywords

Inertial measurement unit; Parameter calibration; Rapid test

Indexed keywords

CALIBRATION; INERTIAL NAVIGATION SYSTEMS; OBJECT RECOGNITION; TESTING;

HIGH ACCURACIES; INERTIAL MEASUREMENT UNIT; INERTIAL MEASUREMENT UNITS; PARAMETER CALIBRATION; PARAMETER CALIBRATIONS; PULSE TIMINGS; RAPID TEST; RAPID TEST METHODS;

ELECTRONIC EQUIPMENT TESTING;

EID: 56849126858     PISSN: 10001328     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (6)

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2. The Series of Missile and Spaceflight. Inertance Element [M]. Beijing: The Astrionics Press, 1996, 6: 195-218.
3. The 13th Institute of CASC. 1C10 IMU Detailed Rules [S]. 2002.
4. The Second Artillery Equipment Academe. Project of Rapid test Technology of IMU [R]. 2003.
5. DENG Zi-li. Optimal Estimate Theory and Application [M]. Harbin: Harbin Industry Press, 2004, 8: 104-142.
6. WU Jun-wei. Estimation of the INS's errors [J]. Journal of Chinese Inertial Technology, 2002, 12 (6).