Second Estimator of the Optimal Quaternion

Journal of Guidance, Control, and Dynamics

Volumn 23, Issue 5, 2000, Pages 885-888

  Mortari, Daniele ^a  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPUTATIONAL COMPLEXITY; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; EIGENVALUES AND EIGENFUNCTIONS; ITERATIVE METHODS; MATRIX ALGEBRA; OPTIMAL CONTROL SYSTEMS; PARAMETER ESTIMATION;

ATTITUDE ESTIMATION ALGORITHMS; SOFTWARE PACKAGE MATLAB;

POSITION CONTROL;

EID: 0034275313     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4618     Document Type: Article

References (15)

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3. Landis Markley, F., and Mortari, D., "How to Estimate Attitude from Vector Observations," AAS/AIAA Astrodynamics Specialist Conf., Paper 99-427, Aug. 1999.
4. Farrell, J. L., Stuelpnagel, J. C., Wessner, R. H., Velman, J. R., and Brock, J. E., "A Least Squares Estimate of Spacecraft Attitude," SIAM Review, Vol. 8, No. 3, 1966, pp. 384-386.
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9. Mortari, D., "Energy Approach Algorithm for Attitude Determination from Vector Observations," Journal of the Astronautical Sciences, Vol. 45, No. 1, 1997, pp. 41-55.
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13. Mortari, D., "ESOQ2 Single-Point Algorithm for Fast Optimal Spacecraft Attitude Determination," Advances in the Astronautical Sciences, Vol. 95, Pt. II, pp. 817-826.
14. Shuster, M. D., "A Survey of Attitude Representations," Journal of Guidance, Control, and Dynamics, Vol. 41, No. 4, 1993, pp. 439-517.
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