Angular-rate estimation using delayed quaternion measurements

1999 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1999, Pages 155-164

  Azor, R ^a   Bar Itzhack, I Y ^b   Deutschmann, J K ^c   Harman, R R ^c  

^a ISRAEL AIRCRAFT INDUSTRIES   (Israel)

^b TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^c NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COVARIANCE MATRIX; DYNAMICS; MARKOV PROCESSES; RICCATI EQUATIONS;

DYNAMICS MODELING; FILTER COVARIANCE; PSEUDO-LINEAR KALMAN FILTER; RATE MEASUREMENTS; ROTATIONAL DYNAMICS; STATE-DEPENDENT ALGEBRAIC RICCATI EQUATIONS; UNIQUE DECOMPOSITION; X-RAY TIMING EXPLORERS;

KALMAN FILTERS;

EID: 84959118162     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-3972     Document Type: Conference Paper

References (15)

1. Harman, R. R., and Bar-Itzhack, I. Y., "Angular-rate Computation Using Attitude Differentiation, " Technical Report No. TAE-881, Faculty of Aerospace Eng., Technion-Israel Institute of Technology, Haifa 32000, Israel, Dec. 97.
2. Harman, R. R., and Bar-Itzhack, I. Y., "The Use of Pseudo-Linear and SDARE Filtering for Satellite Angular-Rate Estimation, " AIAA Guidance, Navigation, and Control Conf., Boston, MA, August 10-12, 1997.
3. Azor, R., Bar-Itzhack, I. Y., and Harman, R. R., "Satellite Angular-rate Estimation from Vector Measurements, " J. of Guidance, Control, and Dynamics, Vol. 21, No. 3, May-June, 1998, pp. 450-457.
4. Natanson, G., "A Deterministic Method for Estimating Attitude from Magnetometer Dáta Only, " Proceedings of the 43rd IFA Congress, Paper No. IFA-92-0036, Washington, DC, Aug. 28-Sept. 5, 1992.
5. 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 Symp., NASA-Goddard Space Flight Center, April 1995.
6. Challa, M., Kotáru, S., and Natanson, G., "Magnetometer-Only Attitude and Rate Estimates During the Earth Radiation Budget Satellite 1987 Control Anomaly, " AIAA Guidance, Navigation, and Control Conf., New Orleans, LA, August 11-13, 1997.
7. Oshman, Y., and Markley, F. L., "Sequential Attitude and Attitude-Rate Estimation Using Integrated-Rate Parameters, " to be published in the J. of Guidance, Control, and Dynamics.
8. Delius, F., "Estimation of Satellite Angular Velocity Using Sequential Measurements of a Single Inertial Vector, " M. Sc. Thesis, Faculty of Aerospace Eng., Technion-Israel Institute of Technology, June 1998. (In Hebrew).
9. Van Bezooijen, R. W. H., "AST Capabilities, " Lockheed Martin Advanced Technology Center, Palo Alto, CA 95304-1191. (Slide presentation).
10. Wertz, J. R., (Ed.), Spacecraft Attitude Dynamics and Control, Reidel Publishing Co., Dordrecht, Holland, 1999.
11. ∞ Control Via the State-Dependent Riccati Equation Technique: Part 1, Theory, " The First International Conf. on Nonlinear Problems in Aviation and Aerospace, Daytona Beach, FL, May 1996.
12. Cloutier, J. R., D’Souza, C. N., and Mracek, C. P., "Nonlinear Regulation and Nonlinear Hm Control Via the State-Dependent Riccati Equation Technique: Part 2, Examples, " The First International Conf. on Nonlinear Problems in Aviation and Aerospace, Daytona Beach, FL, May 1996.
13. Pappano, V., and Friedland, B., "SDRE Observer for an Induction Machine, " The American Control Conf., Albuquerque, NM, June 1997.
14. Mracek, C. P., Cloutier, J. R., and D'Souza, C. N., "A New Technique for Nonlinear Estimation, " IEEE Conf. on Control Applications, Dearborn, MI, September 1996.
15. Gelb, A., (ed.), Applied Optimal Estimation, MIT Press, Cambridge, MA, 1974.