MEMS-based multi-sensor integrated attitude estimation technology for MAV applications

4th IEEE International Conference on Nano/Micro Engineered and Molecular Systems, NEMS 2009

Volumn , Issue , 2009, Pages 1031-1035

  Liang, Xue ^a   Weizheng, Yuan ^a   Honglong, Chang ^a   Chengyu, Jiang ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Attitude estimation; Extended kalman filter; MAV; MEMS sensors; State vector; Stochastic errors

Indexed keywords

ATTITUDE ESTIMATION; MAV; MEMS SENSORS; STATE VECTOR; STOCHASTIC ERRORS;

ACCELEROMETERS; CELLULAR RADIO SYSTEMS; CONTROL THEORY; ESTIMATION; EXTENDED KALMAN FILTERS; GEOMAGNETISM; GYROSCOPES; MEMS; MICROELECTROMECHANICAL DEVICES; MICROSENSORS; POSITION CONTROL; VECTORS;

MEASUREMENT ERRORS;

EID: 70349664764     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/NEMS.2009.5068749     Document Type: Conference Paper

References (13)

1. W. Lidai, x. Shenshu, z. Zhaoying, et aI, "Constrained Filtering Method for MAV Attitude Determination," IEEE Proceedings of the Instrumentation and Measurement Technology Conference, vol. 2, pp. 148-1483, May 2005.
2. Derek B. Kingston, Randal W. Beard, "Real-Time Attitude and Position Estimation for Small UAVs Using Low-Cost Sensors," AIAA 3rd "Unmanned Unlimited" Technical Conference, Workshop and Exhibit, Chicago, Illinois, pp. 1-9, Sep 2004.
3. A. Sharma, M.F. Zaman, M. Zucher, F. Ayazi, "A O.l°/HR bias drift electronically matched tuning fork microgyroscope," Micro Electro Mechanical Systems, 2008, pp. 6-9.
4. L. Yong, Andrew Dempster, L. Binghao, et aI, "A low-cost attitude heading reference system by combination of GPS and magnetometers and MEMS inertial sensors for mobile applications," Journal of Global Positioning Systems, 2006, vol. 5, pp. 88-95.
5. G.H. Elkaim, C. Foster, "MetaSensor: Development of a Low-Cost, High Quality Attitude Heading Reference System," In Institute of Navigation ION GNSS 2006.
6. G. Zhongyu, N. Xiaoji, G. Meifeng, "Quatemion-based Kalman Filter for Micro-machined strapdown attitude heading reference system," Chinese Journal ofAeronautics, 2002, vol. 15, pp. 171-175.
7. Humphreys, T. E., Psiaki, M. L., Klatt, E. M., Powell, S. P., and Kintner, P. M., "Magnetometer-Based Attitude and Rate Estimation for Spacecraft with Wire Booms," Journal of Guidance, Control, and Dynamics, Vol. 28, No.5, 2005, pp. 584-593.
8. C. Hide, T. Moore, M. Smith, "Adaptive Kalman filtering algorithms for integrating GPS and low cost INS," Position Location and Navigation Symposium 2004, pp. 227-233, April 2004.
9. Lam, Q.M., Hunt, T., Sanneman, P., Underwood, S., "Analysis and design of a fifteen state stellar inertial attitude determination system," AIAA Guidance, Navigation, and Control Conference and Exhibit, Austin, Texas, 2003,5483, 11-14.
10. C. Honglong, X. Liang, Q. Wei, Y. Guangmin, Y. Weizheng, "An Integrated MEMS Gyroscope Array with Higher Accuracy Output," Sensors 2008, 8, 2886-2899.
11. Demoz Gebre-Egziabher, Roger C. Hayward and J. David Powell, Design of multi-sensor attitude determination systems, IEEE Transaction on Aerospace and Electronic System 40 (2004) (2), pp. 627649.
12. Caruso M J, "Applications of magnetic sensors for low cost compass systems," IEEE Position Location and Navigation Symposium, 2000, pp. 177-184.
13. Y. Xin, Y. Jixiang, Navigation System, Beijing: Aviation Industry Press, 1993.