Abstract
A principle design is indicated for automatic control of a long range rocket. During the powered flight the rocket is steered by an automatic pilot mounted in the vehicle, according to a prescribed program of motion. If this automatic pilot operates in the right way, the rocket describes its orbit without external intervention. Besides this internal control, the rocket is supervised by a terrestrial station which by radio signals automatically interferes as soon as the rocket deviates from the prescribed orbit, guiding the rocket again into this required trajectory.
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References
J. M. J. Kooy, Principle Electronic Scheme for Automatic Pilot of Long Range Rocket. De Ingenieur (‘s-Gravenhage) 65, No. 20 (1953).
J. M. J. Kooy, Gyroscopes. De Ingenieur (‘s-Gravenhage) 66, No. 17 (1954).
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© 1955 Springer-Verlag Wien
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Kooy, J.M.J. (1955). On Automatic Internal and External Control of Long Range Rockets. In: Hecht, F. (eds) Bericht über den V. Internationalen Astronautischen Kongreß. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-38334-6_12
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DOI: https://doi.org/10.1007/978-3-662-38334-6_12
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-662-37558-7
Online ISBN: 978-3-662-38334-6
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