Research on a new eight-accelerometer configuration for attitude angle calculation of UAV

2010 Chinese Control and Decision Conference, CCDC 2010

Volumn , Issue , 2010, Pages 4119-4123

  Song, Lei ^a   Huang, Chang Qiang ^a   Weng, Xing Wei ^a   Wu, Wen Chao ^a  

^a AIR FORCE ENGINEERING UNIVERSITY   (China)

Author keywords

Accelerometer; Attitude angle calculation; UAV

Indexed keywords

ACCUMULATIVE ERRORS; ATTITUDE ANGLE; ATTITUDE ANGLE CALCULATION; CALCULATION ERROR; CALCULATION PRECISION; DIGITAL SIMULATION; IN-PROCESS; MULTI SENSOR; REDUNDANT INFORMATIONS; TIME ACCUMULATION; UAV;

ACCELEROMETERS;

EID: 77955359963     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/CCDC.2010.5498426     Document Type: Conference Paper

References (6)

1. Jeng-Heng Chen, Sou-Chen Lee,Daniel B DeBra. Gyroscope-free strap down inertial measurement unit by six linear accelerometers[J]. Jorunal of Guidance, Control and Dynamics, 1994, 17(3-4): 286-290.
2. WANG Xiao-na, WANG Shu-zong, ZHU Hua-bing. Study on models of gyroscope-free strap-down inertial navigation systems[J].Acta Armamentarii, 2006, 27(2): 288-292
3. WANG Jin-song, WANG Qi, Shun Sheng-he.Gyro-free inertial measurement unit [J]. Journal of Transducer Technology, 2003, (4): 43-45
4. YIN De-jin, WANG Hong-li, LIU Guang-bin. six-accelerometer configuration for SINS [J]. Journal of Guidance ,Control and Dynamics. 2003, (2): 48-51
5. Chen Zhe. Principles of strap-down inertial navigation systems[M].Beijing: China Astronautics Publishing House,1996
6. WENG Xing-wei. Research on technology of fire and flight control for combined guidance UCAV[D]. Xi'an: Air Force Engineering University, 2008