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Title: Monopulse receiver circuit for an anti-radar missile tracking system

Abstract: 1. In a monopulse radar receiver system for determining the angular co-orates of a pulsed RF radiation source, the combination comprising: An RF signal processing circuit adapted to convert a directional antenna input signals to inversely related pairs of computer input pulses; A pair of automatic gain control pre-amplifiers connected to said processing circuit adapted to simultaneously receive and amplify the pairs of input signals; A difference circuit connected between the outputs of each pair of pre-amplifiers for providing a difference signal pulse; Amplifying means connected with said difference circuit for amplifying said difference signal pulse; A leading-edge gate circuit connected with said amplifying means, adapted to be operatively triggered at the pulse-repetition rate of the pulses propagated by the RF radiation source for accepting only the leading edge of each amplified difference signal pulse; Means for triggering the gate circuit; A pulse integrator circuit connected with the output of said gate circuit adapted to provide an output signal which is a function of the position of the source of radiation; Direct connecting means joining the output of said integrator with one pre-amplifier of said pair for directing the integrator output signal to the one pre-amplifier for dirving the gain thereof in a first direction; An inverter circuit connecting the output of said integrator with the other pre-amplifier of said pair, adapted to invert and combine a reference voltage with the output of said integrator circuit to provide an inverted gain control signal having a reference imposed thereon for driving the gain of the other pre-amplifier in a second direction opposed to said first direction; and A second difference circuit connected with the output of said integrator and the output of said inverter circuit for deriving a difference signal indicative of the angular co-ordinate of the source of pulsed RF radiation, relative to said system, when the difference signal is driven to a zero valve.


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Inventors: Sykes, Langthorne (Manhattan Beach, CA, US)
Russell, Duane J. (China Lake, CA, US)
Atkinson, Robert E. (China Lake, CA, US)

Application Number: 270773
Filing Date: 1963-04-04
Publication_date: 1976-04-13
Assignee: The United States of America as represented by the Secretary of the Navy (Washington, DC)
Primary Class(es): 244/3.19 342/62, 342/149
Other Classes:
US Patent Ref:
2457393Dec, 1948Muffly244/14.
2670158Feb, 1954Philpott244/14.
2935942May, 1960Young et al.244/14.
2969018Jan, 1961Erst et al.244/14.

Other Refs:
Primary Examiner: Hubler, Malcolm F.
Assistant Examiner:
Attorney: Sciascia; R. S., Miller; Roy