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

References
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12 REFERENCES
References preceded by “ # ” have been cited from other references.
MBDA references are not available to the general public
A.1 ARCHER S.M., SWORDER D.D., “Selection of the Guidance Variable for
a Re-Entry Vehicle”, AIAA J. Guidance and Control, Vol. 2, No. 2, 1979,
pp. 130-138.
A.2 #ADLER F.P., “Missile Guidance by 3D Proportional Navigation”,
J. Applied Physics, No. 27, 1956, pp. 500-507.
A.3 ANDRISANI D., KUHL F.P., GLEASON D., “A Nonlinear Tracker Using
Attitude Measurements”, IEEE AES, Vol. 22, No. 5, 1986, pp. 533-539.
A.4 ARCASOY C.C., “The α −β
− γ Tracking Filter with a Noisy Jerk as the
Maneuver Model - Frequency Domain Solution”, IEEE AES, Vol. 32,
No. 3, 1996, pp. 1170-1173.
A.5 ARCASOY C.C., OUYANG G., “Analytical Solution of Tracking Filter
with a Noisy Jerk as Correlated Target Maneuver Model”, IEEE AES,
Vol. 33, No. 1, 1997, pp. 347-353.
B.1 BECKER K., “Closed-Form Solution of Pure Proportional Navigation”, IEE
AES, Vol. 26, No. 3, 1990, pp. 526-533.
B.2 #BEN-ASHER J., YAESH I., “Optimal Guidance with Reduced Sensitivity
to Time-to-go Estimation Errors”, J. Guidance, Vol. 20, No. 1, 1997,
pp. 158-163.
B.3 #BELLMAN R., KAGIWADA H., KALABA R., “Wengert’s Numerical
Method for Partial Derivatives, Orbit Determination, and
Quasilinearization”, Mommun. ACM, No. 8, 1965, pp. 231-232.
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