Passive aircraft and missile detection device

• US 5,828,334 A
• Filed: 05/20/1996
• Issued: 10/27/1998
• Est. Priority Date: 11/10/1994
• Status: Expired due to Fees

• Current Assignee: Thierry Deegan
• Original Assignee: Thierry Deegan
• Inventors: Deegan, Thierry
• Primary Examiner(s): JOHNSON, STEPHEN
• Application Number:
  US08/650,732
• Time in Patent Office: 890 Days
• Field of Search: 342/90, 342/192, 342/193, 342/351, 342/460
• US Class Current: 342/90
• CPC Class Codes: G01S 3/18 derived directly from separate directional antennas
• CPC Class Codes: G01V 3/12 operating with electromagnetic waves operating with millimetre waves G01V8/005

Abstract

This invention offers the capability to passively detect and classify missiles, aircraft, and units with gas turbine engines and rocket motors. It does so by measuring the electromagnetic radiation from ions in the exhaust gas. These emissions are low in frequency and propagate beyond the visual horizon with little attenuation other than through wavefront spreading in the earth-ionosphere waveguide. Acoustic and mechanical processes in combustion chambers and turbines modulate the ion signals in a deterministic manner that makes the engine type classifiable. The proposed passive detection and classification device can sense and identify aircraft, missiles, and potentially ground vehicles and gunfire. This capability will reduce vulnerability of forces to threats and reduce fratricide among friendly units.

Claims

1. A method of passively detecting aircraft and missiles having engines which form exhaust streams by measuring the electromagnetic emissions caused by accelerating ions that have been generated by combustion in the engines of said aircraft and missiles, wherein related spectral features of said measured emissions are used to classify the distinctive type of said engine, said spectral features being indicative of the number of turbine blades, stator vanes, chamber geometry, nozzle ratio and dynamic properties of said engine.

2. A method of passively detecting aircraft and missiles having engines which form exhaust streams by measuring the electromagnetic emissions caused by accelerating ions that have been generated by combustion in the engines of said aircraft and missiles, wherein the spectral features of said measured emissions are related to a library of similar signals from known sources to classify the emissions as emanating from a threat or non-threat aircraft.

3. A passive aircraft detection device, comprising:

a means of sensing the electromagnetic emissions from accelerated combustion ions;

a means of measuring the energy level of said emissions in the frequency regime of said ions accelerated by exhaust turbulence, turbine blade modulation, and engine resonances;

a means of measuring the frequency content of said emissions in the frequency regime of said ions accelerated by said turbine blade modulation and said engine resonances; and

a means to relate said emission energy levels and measured frequencies to previously measured emissions so as to identify the fact that said emissions are from a combustion engine.

4. The passive aircraft detection device of claim 3 that also provides classification information, said device comprising the elements of claim 3 and further comprises a means to correlate said emission energy levels and frequency measurements to previously measured emission signal patterns so as to identify the type of engine generating said emissions.

5. The passive aircraft detection device of claim 3 in which said measured combustion ion emission signals have a direction of arrival to said device which direction of arrival corresponds to the direction of said emitting engine to said device, said device also providing direction-finding information, said device comprising the elements of claim 3 and further comprises a means to determine the direction of arrival of said measured combustion ion emission signals so as to determine the direction to said emitting engine from said detection device.

6. The method of passively detecting aircraft and missiles by measuring the electromagnetic emissions caused by accelerating ions chemically generated in engine combustion to determine the frequency spectrum of such emissions and thereafter relating said spectrum to frequencies representative of cyclotron emissions from combustion ions, engine resonances, exhaust jet turbulence, and engine turbine blade-rate modulations of the jet to determine the presence or non-presence of said aircraft or said missile, wherein related features of the broadband spectrum of jet turbulence, modulations due to resonances in the combustion chamber and nozzle, and narrowband blade-rate frequencies superimposed on the jet are compared with a library of similar signals from known sources to classify the engine type of the source.

7. The method of passively detecting aircraft and missiles by measuring the electromagnetic emissions caused by accelerating ions chemically generated in engine combustion to determine the frequency spectrum of such emissions and thereafter relating said spectrum to frequencies representative of cyclotron emissions from combustion ions, engine resonances, exhaust jet turbulence, and engine turbine blade-rate modulations of the jet to determine the presence or non-presence of said aircraft or said missile and wherein said electromagnetic emissions have a direction of arrival corresponding to the direction of said aircraft and missiles to the receiver, and further measuring said direction of arrival of said electromagnetic emissions so as to determine the direction of said aircraft or said missile from said receiver.