Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1976-04-19
1978-12-26
Engle, Samuel W.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
343 16R, 343 16M, F41G 700, F41G 718, G01S 902
Patent
active
041312546
ABSTRACT:
A proportional processing technique having a wide instantaneous dynamic range and providing a significant increase in instantaneous dynamic range over presently known proportional processing methods. These improvements are made possible by the use in accordance with this invention of a logarithmic amplifier in each channel of a pair of channels relatable to the same sensing plane. Each logarithmic amplifier is preferably arranged to operate substantially at the midpoint of its operating characteristic, and the pair of channels may be orthogonally related to another pair of channels, such that suitable guidance commands can be derived and furnished for example to a missile.
REFERENCES:
patent: 3012222 (1961-12-01), Hagemann
patent: 3064252 (1962-11-01), Varela
patent: 3089136 (1963-05-01), Albersheim
patent: 3342984 (1967-09-01), Gray et al.
Introduction to Monopulse pp. 50-51 (1959).
Analog Computation by Albert S. Jackson, pp. 482 to 489, McGraw-Hill Book Co., Inc. (1960).
Chin Gay
Eisel James B.
Engle Samuel W.
Martin Marietta Corporation
Renfro Julian C.
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