A Complementary Filter for High-fidelity Attitude Estimation based on Decoupled Linear/Nonlinear Properties of Inertial Sensors

Author:

Sugihara Tomomichi,Masuya Ken,Yamamoto Motoji

Publisher

The Robotics Society of Japan

Reference15 articles.

1. [1] E.J. Lefferts, F.L. Markley and M.D. Shuster: “Kalman Filtering for Spacecraft Attitude Estimation,” Journal of Guidance, Control and Dynamics, vol.5, no.5, pp.417–429, 1982.

2. [2] G. Creamer: “Spacecraft Attitude Determination Using Gyros and Quaternion Measurements,” The Journal of the Astronautical Sciences, vol.44, no.3, pp.357–371, 1996.

3. [3] X. Yun, C. Aparicio, E.R. Bachmann and R.B. McGhee: “Implementation and Experimental Results of a Quaternion-Based Kalman Filter for Human Body Motion Tracking,” Proceedings of the 2005 IEEE International Conference on Robotics and Automation, pp.317–322, 2005.

4. [5] W.H. Wirkler: Aircraft Course Stabilizing Means, U.S. Patent 2, 548, 278, 1951-04-10.

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