Kalman filter divergence and aircraft motion estimators

Journal of Guidance, Control, and Dynamics

Volumn 1, Issue 1, 1978, Pages 71-79

  Bryson, Arthur E ^a  

^a STANFORD UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85003383717     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.55745     Document Type: Article

References (11)

1. Luenberger, D.G., “Observing the State of a Linear-System,” IEEE Transactions on Military Electronics, Vol. 8, April 1964, pp. 7480.
2. Battin, R.H. and Levine, G.M., “Applications of Kalman Fitering Techniques in the Apollo Program,” NATO AGARD-ograph 139, Feb. 1970.
3. Breza, M.J. and Bryson, A.E., “Minimum-Variance Steady-State Filters with Eigenvalue Constraints,” Proceedings of the 5th Symposium on Nonlinear Estimation, San Diego, Sept. 1974.
4. Cannon, R.FI. Jr., Dynamics of Physical Systems, McGraw-Hill, New York, 1967, pp. 409-418.
5. Schmidt, S.F., “Computational Techniques in Kalman Filtering,” NATO AGARD-ograph 139, Feb. 1970.
6. Anderson, B.D.O. and Moore, J.B., Linear Optimal Control, Prentice Hall, Englewood Cliffs, N.J., 1971.
7. Bryson, A.E. and Ho, Y.C., Applied Optimal Control, Hemisphere Pub. Co., Washington, D.C., 1975.
8. Holley, W.E. and Bryson, A.E., “Wind Modeling and Lateral Control for Automatic Landing,” Journal of Spacecraft and Rockets, Vol. 14, Feb. 1977, pp. 65-72.
9. Teper, G.L., “Aircraft Stability and Control Data,” Systems Tech. Inc., Hawthorne, Calif., TR 176-1, April 1969.
10. Hall, W.E., “Computational Methods for the Synthesis of Rotary-Wing VTOL Aircraft Control Systems,” Ph.D. Dissertation, Stanford University, Aug. 1971.
11. Luenberger, D.G., Introduction to Linear and Nonlinear Programming, Addison-Wesley, Reading, Mass., 1973.