Quaternion-Based Kalman Filter for Micro-machined Strapdown Attitude Heading Reference System

Author:

GAO Zhong-yu,NIU Xiao-ji,GUO Mei-feng

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference4 articles.

1. Zhang R, Gao Z, Chen Z. Bulk micromachined vibrating wheel rate gyroscope[A]. In: Norman C T ed. Proceedings of SPIE - The International Society for Optical Engineering [C]. Nanjing, 2001. 54–58.

2. Design of a multi-finger silicon micromechanical accelerometer[J];Yuan;Journal of T singhua University,1998

3. Spacecraft attitude determination using gyro and quaternion measurements[J];Creamer;The Journal of Astronautical Science,1996

4. Gebre-Egziabher D, Elkaim G H, Powell J D, et al. A gyro-free quaternion-based attitude determination system suitable for implementation using low cost sensors [A]. In: IEEE PLANS, Position Location and Navigation Symposium[C]. IEEE, 2000. 185–192.

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