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

References
_ _
L.2 LOOZE D.P., HSU J.Y., GRUNBERG D., “Investigation of the Use of
Acceleration Estimates by Endgame Guidance Laws”, AIAA J. Guidance
and Control, Vol. 13, No. 2, 1990, pp. 198-206.
L.3 LEE G.K.F., “Estimation of the Time-to-Go Parameter for Air-to-Air
Missiles”, J. Guidance, Control and Dynamics, Vol. 8, No. 2, 1985, pp. 262-
266.
L.4 LEE G.T., LEE J.G., “Improved Command to Line-of-Sight for Homing
Guidance”, IEEE AES, Vol. 31, No. 1, 1995, pp. 506-510.
L.5 LI X.R., ZHANG Y., “Numerically Robust Implementation of Multiple-
Model Algorithms”, IEEE AES, Vol. 36, No. 1, 2000, pp. 266-278.
L.6 LONGBIN M., XIAOQUAN S., YIYU Z., KANG S.Z., “Unbiased
Converted Measurements for Tracking”, IEEE AES, Vol. 34, No. 3, 1998,
pp. 1023-1027.
L.7 LERRO D., BAR-SHALOM Y., “Tracking with Debiased Consistent
Converted Measurements Versus EKF”, IEEE AES, Vol. 29, No. 3, 1993,
pp. 1015-1022.
L.8 LOBBIA R., KENT M., “Data Fusion of Decentralised Local Tracker
Outputs”, IEEE AES, Vol. 30, No. 3, 1994, pp. 787-798.
L.9 LAMBERT W.D., SWICK C.H., "Formulas and Tables for the Computation
of Geodetic Positions of the International Ellipsoid", Special Publication
200, U.S. Coast and Geodetic Survey, Washington, 1935, pp. 26.
L.10 LAWRENCE A., “Modern Inertial Technology - Navigation, Guidance and
Control”, ISBN 0-387-97868-2, 1993.
12-8
M
M.1 MAHAPATRA P.R., SHUKLA U.S., “Accurate Solution of Proportional
Navigation for Maneuvering Targets”, IEEE AES, Vol. 25, No. 1, 1989,
pp. 81-89.
M.2 MAZOR E., AVERBUCH A., BAR-SHALOM Y., DAYAN J., “Interacting
Multiple Model Methods in Target Tracking: A Survey”, IEEE AES,
Vol. 34, No. 1, 1998, pp. 103-123.
M.3 #MAGILL D.T.,”Optimal Adaptive Estimation of Sampled Stochastic
Processes”, IEEE AC., Vol. 10, 1965, pp. 434-439.