AN IMPROVED COMPLEMENTARY FILTER ALGORITHM IN THE APPLICATION OF THE MOBILE ROBOT ATTITUDE ESTIMATION, 163-169.

Zhaihe Zhou, Jiajie Fu, Jianxin Lv, and Qianyun Zhang

References

  1. [1] V. Kumar, D. Rus, and S. Singh, Robot and sensor networksfor first responders, IEEE Pervasive Computing, 3(4), 2004,24–33.
  2. [2] J. Debruin, Control systems for mobile satcom antennas,Control Systems IEEE, 28(1), 2008, 86–101.
  3. [3] K. Bohm and K. Perermann, Signal processing schemes for the fiber-optic gyroscope, Cambridge Symposium-Fiber/lase, NewYork, NY, USA, 1987, 36–44.
  4. [4] A.J. Baerveldt and R. Klang, A low-cost and low-weightattitude estimation system for an autonomous helicopter, IEEEInt. Conf. on Intelligent Engineering Systems, 1997 (INES’97),Budapest, Hungary, 1997, 391–395.
  5. [5] V. Cern´y and J. Hrusak, Comparing frequency domain, optimal, and asymptotic filtering: A tutorial, Control and Intelligent Systems, 34(2), 2006, 136.
  6. [6] M. Won and S.S. Kim, Design and control of a marine satelliteantenna, Journal of Mechanical Science and Technology, 19(1),2005, 473–480.
  7. [7] T.L. Chia, D. Simon, and H.J. Chizeck, Kalman filtering withstatistical state constraints, Control & Intelligent Systems,34(1), 2008, 73–79.
  8. [8] D.J. Jwo and C.N. Lai, Unscented Kalman filter with nonlineardynamic process modeling for GPS navigation, GPS Solutions,12(4), 2008, 249–260.
  9. [9] S. Ma and L. Wei, Non-linear PID control method with feed-forward in smart car, Proc. of 2009 Control and DecisionConference, Vol. 1, Guilin, Guangxi, China, 2009, 462–465.
  10. [10] J.K. Lee, E.J. Park, and S.N. Robinovitch, Estimation of attitude and external acceleration using inertial sensor measurement during various dynamic conditions, IEEE Transactionson Instrumentation & Measurement, 61(8), 2012, 2262.
  11. [11] S. Miah and W. Gueaieb, Mobile robot navigation usingdirection-sensitive RFID reader, Control & Intelligent Systems,39(39), 2011, 254–264.
  12. [12] X. Ruan, J. Liu, H. Di, X. Li, and J. Zhao, System design,modeling and LQ control of a two-wheeled self-balancing robot,Modern Electronics Technique, 18(281), 2008, 57–60.
  13. [13] D. Jung and P. Tsiotras, Inertial attitude and position reference system development for a small UAV, AIAA Infotech atAerospace, 2007, 7–10.
  14. [14] D. Gebre-Egziabher, R.C. Hayward, and J.D. Powell, Designof multi-sensor attitude determination systems, IEEE Trans-actions on Aerospace and Electronic Systems, 40(2), 2004,627–649.
  15. [15] S.C. Stubberud and K.A. Kramer, Predictive guidance intercept using the neural extended Kalman filter tracker, Control& Intelligent Systems, 35(3), 2007, 228–235.
  16. [16] R. Mahony, T. Hamel, and J.M. Pflimlin, Complementaryfilter design on the special orthogonal group SO(3), Decisionand Control, 2005 and 2005 European Control Conference.CDC-ECC’05, 2006, 1477–1484.
  17. [17] R. Mahony, T. Hamel, P. Morin, and E. Malis, Nonlinearcomplementary filters on the special linear group, InternationalJournal of Control, 85(10), 2012, 1557–1573.
  18. [18] Y.S. Suh, Attitude estimation using low cost accelerometer andgyroscope, The 7th Korea-Russia Int. Symp. on Science andTechnology, Univ Ulsan, Ulsan, South Korea, 2003, 423–427.
  19. [19] J. Jarrell, G. Yu, B. Seanor, and M. Napolitano, Aircraftattitude, position, and velocity determination using sensorfusion, AIAA Guidance, Navigation and Control Conferenceand Exhibit, 2006, 18–21.
  20. [20] X.W. Shen, M.L. Yao, and P. Zhao, Antenna attitude estimation based on complementary filter for mobile satellitecommunication, Journal of Chinese Inertial Technology, 19(2),2011, 194–197.

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