Analysis and design of a fifteen state stellar inertial attitude determination system

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Lam, Quang M ^a   Hunt, Teresa ^a   Sanneman, Paul ^a   Underwood, Stanley ^a  

^a Guidance Navigation and Control Group ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE DETERMINATION; ATTITUDE DETERMINATION SYSTEMS; CALIBRATION FILTERS; DESIGN AND DEVELOPMENT; MISALIGNMENT MATRIX; OPERATING CONDITION; SCALE FACTOR ERRORS; SCALE FACTOR STABILITY;

CALIBRATION; GYROSCOPES;

DESIGN;

EID: 84896882831     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

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2. Deutschmann, J. and Bar-Itzhack, I. Y., 'Extended Kalman Filter for Attitude Estimation of the Earth Radiation Budget Satellite," NASA CP-3050, Flight Mechanics and Estimation Theory Symposium, Greenbelt MD, May 10-11, 1989
3. Bar-Itzhack, I. Y., Deutschmann, J., and Markley, F. L., "Quaternion Normalization in Additive EKF for Spacecraft Attitude Determination," AIAA Astrodynamics Specialist Conference, Monetery, CA August 2002
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8. Markley, L. F., "Attitude Error Representation for Kalman Filtering," Journal of Guidance, Control, and Dynamics, March-April 2003
9. Murrell, J. W., "Precision Attitude Determination for Multi-mission Spacecraft," AIAA GN&C Conference, 1978.
10. R. L. Farenkopf, "Generalized Results for Precision Attitude Reference Systems Using Gyros," AIAA Paper No. 74-903, AIAA Mechanics and Control of Flight Conference, August 5-9, 1974
11. R. Brown & P. Hwang, Introduction to Random Signals and Applied Kalman Filtering, John Wiley & Sons, 1985