Quaternion attitude estimation using vector observations

Journal of the Astronautical Sciences

Volumn 48, Issue 2-3, 2000, Pages 359-380

  Markley, F L ^a   Mortari, D ^a  

^a NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; EIGENVALUES AND EIGENFUNCTIONS; MAXIMUM LIKELIHOOD ESTIMATION; POLYNOMIALS; SPACE FLIGHT; VECTORS; AEROSPACE ENGINEERING; ASTRONOMY;

ESTIMATORS OF THE OPTIMAL QUATERNION; QUATERNION ATTITUDE ESTIMATION; QUATERNION ESTIMATOR; SINGULAR VALUE DECOMPOSITION; WAHBAS LOSS FUNCTION;

SPACECRAFT; SINGULAR VALUE DECOMPOSITION;

ATTITUDE ESTIMATION; COMPUTATIONAL BURDEN; LOSS FUNCTIONS; MULTIPLE STARS; NEW RESULTS; SEQUENTIAL ROTATIONS; SINGULAR VALUE DECOMPOSITION METHOD; VECTOR OBSERVATIONS;

EID: 0034165598     PISSN: 00219142     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Conference Paper

References (27)

1. A least squares estimate of spacecraft attitude
2. Maximum likelihood estimate of spacecraft attitude
3. A least squares estimate of spacecraft attitude
4. Attitude determination using vector observations and the singular value decomposition
5. Attitude determination using vector observations and the singular value decomposition
6. Analysis of least-squares attitude determination routine DOAOP
7. Three-axis attitude determination
8. Parameterizations of the attitude
9. A survey of attitude representations
10. Attitude determination using vector observations: A fast optimal matrix algorithm
11. Approximate algorithms for fast optimal attitude computation
12. Three-axis attitude determination from vector observations
13. Quaternion computation from a geometric point of view
14. New quaternion attitude estimation method
15. Euler-q algorithm for attitude determination from vector observations
16. ESOQ: A closed-form solution to the Wahba problem
17. n-dimensional cross product and its application to matrix eigen-analysis
18. ESOQ2 single-point algorithm for fast optimal attitude determination
19. Second estimator of the optimal quaternion
20. Comparison of single frame attitude determination methods