Thesis - Leigh Moody.pdf - Bad Request - Cranfield University

Bibliography
_ _
S.47 SPEYER J.L., CRUES E.Z., “On-Line Aircraft State and Stability
Derivative Estimation Using Modified-Gain Extended Kalman Filter”,
AIAA J. Guidance and Control, Vol. 10, No. 3, 1987, pp. 262-268.
S.48 SPEYER J.L., GUSTAFSON D.E., “An Approximation for Estimation in
Linear Systems with Parameter Uncertainty”, IEEE AC., Vol. 20, No. 6,
1975, pp. 354-359.
S.49 SPEYER J.L., HULL D.G., “Comparison of Several Extended Kalman
Filter Formulations for Homing Missile Guidance”, Proc. of AIAA
Guidance and Control Conference, Massachusetts, August 1988.
S.50 SPINGARN K., WEIDEMANN H.L., “Linear Regression Filtering and
Prediction for Tracking Maneuvering Aircraft Targets”, IEEE AES, Vol. 8,
November 1972, pp. 800-810.
S.51 STATMAN J.I., “Simplified Solution for a Class of Fading Memory
Filters”, IEEE AES, Vol. 23, No. 3, 1987, pp. 355-360.
S.52 STURZA M.A., “GPS Navigation Using Three Satellites and a Precise
Clock”, J. ION, Vol. 30, No. 2, 1983, pp. 146-156.
S.53 SUN J.L., “How to Perform Differentiations on Matrices”, AIAA
J. Guidance and Control, Vol. 13, No. 5, 1990, pp. 924-926.
S.54 SWERLING P., PETERMAN W.L., “Radar Measurement Accuracy for
Fluctuating Targets”, IEEE AES, Vol. 27, No. 6, 1991, pp. 868-870.
S.55 SWERLING P., “Radar Probability of Detection for Some Additional
Fluctuating Target Cases”, IEEE AES, Vol. 33, No. 2, 1997, pp. 698-709.
S.56 SWORDER D.D., KENT M., VOJAK R., HUTCHINS R.G., “Renewal
Models for Maneuvering Targets”, IEEE AES, Vol. 31, No. 1, 1995,
pp. 138-150.
S.57 SWORDER D.D., WELLS G.R., “Guidance Laws for Aerodynamically
Controlled Re-entry Vehicles”, J. Spacecraft, Vol. 14, No. 2, 1977, pp. 111-
117.
S.58
S.59
# SONG T-L, SPEYER J., “The Modified Gain Extended Kalman Filter and
Parameter Identification in Linear Systems”, Automatica, Vol. 22, No. 1,
1986.
# SONG T-L, LEE D-G, “Effective Filtering of Target Glint”, IEEE AES,
Vol. 36, No. 1, 2000, pp. 234-240.
13-24