Double sideband linear frequency modulation system for radar applications

• US 4,388,622 A
• Filed: 04/15/1981
• Issued: 06/14/1983
• Est. Priority Date: 04/15/1981
• Status: Expired due to Fees

• Current Assignee: United States Of America As Represented By The Secretary Of The Army (Government of the United States of America)
• Original Assignee: The United States Of America As Represented By The Secretary Of The Army
• Inventors: Fletcher, Robert H. Jr.
• Primary Examiner(s): Wilbur, Maynard R.
• Assistant Examiner(s): Burk, Robert C.
• Application Number:
  US06/254,237
• Time in Patent Office: 790 Days
• Field of Search: 343/14, 343/9 R, 343/17.5, 343/17.2 PC, 343/5 NQ
• US Class Current: 342/112
• CPC Class Codes: G01S 13/343 using sawtooth modulation
• CPC Class Codes: G01S 13/347 using more than one modulation frequency
• CPC Class Codes: G01S 13/58 Velocity or trajectory determination systems; Sense-of-movement determination systems

Abstract

A double sideband linear frequency modulation technique for radar applications is disclosed for obtaining simultaneous range and doppler measurements. The method of obtaining measurements is useful in a variety of radar applications; however, the most promising area is in continuous wave radar systems. Linear Frequency Modulated (LFM) waveforms of both increasing and decreasing frequency are simultaneously transmitted. Upon reception, these sideband signals are combined coherently to give an output that is a function of the target'"'"'s radial velocity. The received signals are also processed separately to obtain target ranging information.

Claims

1. In a radar system wherein a continuous wave of electromagnetic energy is transmitted toward an object and reflected energy is received from the object, the improvement of a double sideband linear frequency modulation system comprising:

transmitting means providing upper and lower sidebands of a carrier signal with simultaneously increasing and decreasing transmitted frequency waveforms;

receiving means adapted for receiving reflected portions of said transmitted waveforms, and for separating said reflected portions into said upper and lower sidebands of said carrier signal, said upper and lower portions of reflected energy having both range and doppler signal components therein simultaneously; and

signal processing means for coherently combining the reflected sideband portions for separating the range and doppler signal components, said signal processing means comprising a first mixer having inputs adapted for receiving said reflected sideband portions for providing a sideband sum output, and a notch filter responsive to said sum output for eliminating clutter and thereby enhancing the frequency component of the signal output therefrom for determining radial velocity of the object.

2. A double sideband linear frequency modulation system as set forth in claim 1 wherein said signal processing means further comprises first and second band rejection filters having inputs coupled selectively to respective first mixer inputs, said first filter being coupled to receive said upper reflected sideband signal and said second filter being adapted to receive said lower reflected sideband signal for rejecting stationary clutter returns in the respective sidebands and thereby enhancing the signal frequency outputs therefrom for determining object range.

3. A double sideband linear frequency modulation system as set forth in claim 2 wherein said signal processing means further comprises a first bandpass filter coupled between the output of said first mixer and the notch filter, and a second mixer having a first input adapted for receiving the output of the notch filter;

and said modulation system further comprising an offset oscillator circuit for providing selectable oscillator frequency outputs to said signal processing means, a first output of said offset oscillator circuit being coupled as a second input of said second mixer for mixing with said sum output of the notch filter to provide in-phase and quadrature channel output signals therefrom for obtaining said radial velocity of the object.

4. A double sideband linear frequency modulation system as set forth in claim 3 wherein said signal processing means further comprises third and fourth mixers coupled to receive respective first inputs from said first and second band reject filters outputs, coupled to receive respective second inputs from a second output of said offset oscillator for mixing the respective sideband signals to baseband.

5. A double sideband linear frequency modulation system as set forth in claim 4 and further comprising fifth and sixth mixers, means for coupling a portion of said upper and lower modulated sidebands from said transmitting means to respective first inputs of said fifth and sixth mixers, said offset oscillator second output being further coupled to the second inputs of said fifth and sixth mixers, second and third bandpass filters responsive to outputs of said fifth and sixth mixers respectively for providing a sideband output from each filter, seventh and eighth mixers having respective first inputs coupled to the respective outputs of said second and third bandpass filters, said seventh and eighth mixers having second inputs adapted for receiving respectively said reflected portions of said upper sideband and lower sideband of said carrier signal, and fourth and fifth bandpass filters having respective inputs coupled to the respective outputs of said seventh and eighth mixers for providing outputs as said first mixer inputs and said band rejection filter inputs.

6. In a radar system wherein a continuous wave of high frequency electromagnetic energy is transmitted toward an object and reflected energy is received from the object, the method of simultaneously processing both object range and doppler signal components coincident in a reflected energy waveform and comprising the steps of:

mixing a carrier signal frequency with a linear frequency modulator output signal and filtering the resultant mixed output for obtaining respective upper and lower modulated sideband waveforms in separate channels;

combining said sideband waveforms so that the upper sideband is increasing and the lower sideband is decreasing simultaneously at a linear frequency modulation rate;

transmitting the combined waveforms toward an object;

receiving portions of the combined waveforms reflected from an object;

filtering the received waveforms into the respective upper and lower sidebands in separate channels;

continuously mixing a reference signal portion of the transmitted upper and lower sidebands with respective upper and lower received sideband portions;

passing the continuously mixed upper sideband signal portion and continuously mixed lower sideband signal portion through respective bandpass filters and band rejection filters for removing clutter and providing ranging signals;

recombining portions of said continuously mixed lower sidebands and upper sidebands after passage of these signals through said bandpass filters and before passage through said band rejection filters for providing a summation signal output; and

processing said summation signal through a bandpass filter and a notch filter to selectively obtain the frequency components comprising the in-phase and quadrature components for providing the object radial velocity.

7. The method of simultaneously processing both object range and doppler signal components coincident in a reflected waveform as set forth in claim 6 and further comprising the step of mixing an offset oscillator frequency with said reference signal portions of the respective upper and lower transmitted sidebands and filtering the mixed outputs thereof prior to combining the transmitted and received sideband portions.