Rate estimator for windowed quaternion estimator

Advances in the Astronautical Sciences

Volumn 112 I, Issue , 2002, Pages 73-84

  Kim, Injung ^a   Kim, Jinho ^b   Kim, Youdan ^a  

^a Seoul National University   (South Korea)

^b GNC Group   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DIFFERENTIAL EQUATIONS; KINEMATICS; PERTURBATION TECHNIQUES; SPACECRAFT;

STATE OBSERVER; STATE TRANSITION MATRICES; WINDOWED QUATERNION ESTIMATOR;

AEROSPACE ENGINEERING;

EID: 0036910543     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. F. L. Markley and D. Mortari, "How To Estimate Attitude From Vector Observations," Proceedings of the AAS/AIAA Astrodynamics Conference, AAS 99-427, Girdwood, Alaska, August 16-19, 1999, pp.1979-1996.
2. G. Wahba, "A Least Squares Estimate of Spacecraft Attitude", SIAM Review, Vol. 7, No. 3, July 1965, p. 409.
3. M. D. Shuster and S. D. Oh, "Three-Axis Attitude Determination From Vector Observations", Journal of Guidance and Control, Vol. 4, No. 1, January-February 1981, pp. 70-77.
4. I. Kim, J. Kim, C. Park and S. Rhee, "Attitude Determination Using Windowed Quaternion Estimator," AAS 01-381 AAS/AIAA Astrodynamics Specialists Conference, Quebec City, Quebec, Canada, July 30 - August 2, 2001.