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Theoretical Principles of Guided Missile Systems*

Published online by Cambridge University Press:  04 July 2016

E. G. C. Burt*
Affiliation:
Guided Weapons Department, Royal Aircraft Establishment, Farnborough

Extract

A guided missile system is a very complex assembly of interacting sub-systems, and rarely fits into a neat mathematical framework; but the need for a sound theoretical background is perhaps even more acute in this than in other fields, because of the almost prohibitive cost of protracted experimentation and cut-and-try methods. A theoretical model—even an approximate one—can greatly reduce the amount of experimental work necessary to prove a system, since the less efficient arrangements can be eliminated without a shot being fired. The use of simulators and computers, although indispensable, is in no way a substitute for this theoretical understanding: for the computer solutions can be obtained only for specific cases, and are of limited use unless they can be generalised to apply to other situations.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1959

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Footnotes

*

The Eighth Lecture to be given to the Astronautics and Guided Flight Section of the Society—on 19th February 1959.

References

1.Wiener, N. (1949). Extrapolation, Interpolation and Smoothing of Stationary Time Series. Wiley, New York, 1949.Google Scholar
2.Burt, E. G. C. (1956). Self-optimising Systems. Proceedings of Conference on Automatic Control, Heidelberg, 1956.Google Scholar
3.Roberts, A. P. (1959). Self-optimising control systems for a certain class of randomly varying inputs. Paper read to the Society of Instrument Technology, 16th April 1959.Google Scholar