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

Bibliography
_ _
K.28 KOVACEVIC F., “Microprocessor Control of Rocket Flight Stabilization”,
Microprocessors and Microsystems, Vol. 11, No. 6, 1987, pp. 330-336.
K.29 KUMAR R., KELLEY H.J., “Singular Optimal Atmospheric Rocket
Trajectories”, AIAA J. Guidance and Control, Vol. 11, No. 4, 1988,
pp. 305-312.
K.30 KOCH W., “Fixed-Interval Retrodiction Approach to Bayesian IMM-MHT
for Maneuvering Multiple Targets”, IEEE AES, Vol. 36, No. 1, 2000, pp. 2-
14.
K.31 KIM K.B., KIM M-J, CHOI J.W., “Modified Receding Horizontal
Guidance Law with Information on Small Accurate Time-to-Go”, IEEE
AES, Vol. 36, No. 2, 2000, pp. 725-729.
K.32 KRONHAMN T.R., Geometric Illustration of the Kalman Filter Gain and
Covariance Update Algorithms”, IEEE Control Systems Magazine, May
1985, pp. 41-43.
L.11 LARGE E., “Optimal Flight Paths for a Winged Supersonic Rocket
Vehicle”, Aeronautical Journal, December 1978, pp. 517-522.
L.12 LASSITER E.M., PARKINSON B., “The Operational Status of
NAVSTAR/GPS”, J. Navigation, Vol. 30, No. 1, pp. 35-47.
L.13 LEFFERTS R.E., “Alpha-Beta Filters in Polar Coordinates with
Acceleration Corrections”, IEEE AES, Vol. 24, No. 6, 1988, pp. 693-699.
L.14 LEE A.Y., “Optimal Autorotation Descent of a Helicopter with Control and
State Inequality Constraints”, AIAA J. Guidance and Control, Vol. 13,
No. 5, 1990, pp. 922-924.
L.15 LEE G.T., LEE J.G., ROH Y.K., PARK C.G., “Modeling Quaternion Errors
in SDINS: Computer Frame Approach”, IEEE AES, Vol. 34, No. 1, 1998,
pp. 289-299.
L.16 LEE Y.C., “New Concept for Independent GPS Integrity Monitoring”,
J. ION, Vol. 35, No. 2, pp. 239-253.
L.17 LEE Y.C., “Ground Monitoring Schemes for GPS Integrity Channel”, IEEE
AES, Vol. 26, No. 3, pp. 481-489.
L.18 LEFAS C.C., “Real-Time Wind Estimation and Tracking with Transponder
Downlinked Airspeed and Heading Data”, IEEE AES, Vol. 23, No. 2, 1987,
pp. 169-173.
13-15
L