Satellite angular rate estimation from vector measurements

1996 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1996, Pages 1-10

  Azor, Ruth ^a   Bar Itzhack, Itzhack Y ^b,c   Harman, Richard P ^b  

^a ISRAEL AIRCRAFT INDUSTRIES   (Israel)

^b Flight Dynamics Support Branch   (Israel)

^c TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

DIFFERENTIAL EQUATIONS; NONLINEAR DYNAMICAL SYSTEMS; NONLINEAR EQUATIONS; SATELLITES;

ANGULAR RATE; NONLINEAR DIFFERENTIAL EQUATION; SATELLITE DATA; THREE-DIMENSIONAL BODY; TIME DERIVATIVE; VECTOR MEASUREMENTS;

KALMAN FILTERS;

EID: 84959137802     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3751     Document Type: Conference Paper

References (7)

1. Natanson, G., “A Deterministic Method for Estimating Attitude from Magnetometer Data Only,” Proceedings of the 43rd IFA Congress, Paper No. IFA-92-0036, Washington, DC, Aug. 28 - Sept. 5, 1992.
2. Challa, M., Natanson, G., Deutschmann, J., and Galal, K., “A PC-Based Magnetometer-Only Attitude and Rate Determination System for Gyroless Spacecraft,” Proceedings of the Flight Mechanics/Estimation Theory Symposium, NASAGoddard Space Flight Center, May 16-18, 1995. pp. 83-96.
3. Gelb, A., (ed.), Applied Optimal Estimation, MIT Press, Cambridge, MA, 1974, p. 19.
4. Algrain, M. C., and Saniie, J., “Interlaced Kalman Filtering of 3-D Angular Motion Based on Ruler's Nonlinear Equations,” IEEE Trans. on Aerosp. And Elect. Sys., Vol. 30, No. 1, 1994, pp. 175-185.
5. Wertz, J. R., (Ed.), Spacecraft Attitude Dynamics and Control, Reidel Publishing Co., Dordrecht, Holland, 1999, p. 523.
6. Agrawal, B. N., Design of Geosynchronous Spacecraft, Prentice-Hall, Englewood, NJ, 1999. p. 109.
7. Meriam, J.L., and Kraige, L.G., Engineering Mechanics Volume 2, Dynamics. Wiley, New-York, NY, 1992, pp. 383-386.