Gated FMCW DF radar and signal processing for range/doppler/angle determination

• US 5,361,072 A
• Filed: 02/28/1992
• Issued: 11/01/1994
• Est. Priority Date: 02/28/1992
• Status: Expired due to Term

• Current Assignee: CODAR Ocean Sensors Ltd.
• Original Assignee: CODAR Ocean Sensors Ltd.
• Inventors: Lilleboe, Peter M., Isaacson, Jimmy, Barrick, Donald E., Lipa, Belinda J.
• Primary Examiner(s): Hellner, Mark
• Application Number:
  US07/843,183
• Time in Patent Office: 977 Days
• Field of Search: 342/432, 342/13, 342/107, 342/133, 342/175, 342/196, 343/793
• US Class Current: 342/133
• CPC Class Codes: G01S 13/0218 Very long range radars, e.g. surface wave radar, over-the-horizon or ionospheric propagation systems for meteorological use G01S13/95
• CPC Class Codes: G01S 13/42 Simultaneous measurement of distance and other co-ordinates indirect measurement G01S13/46
• CPC Class Codes: G01S 7/35 Details of non-pulse systems

Abstract

A lower-frequency compact radar system for wide-angle surveillance. Direction-finding receive antennas consisting of colocated orthogonal electric and magnetic dipoles provide target angles from the radar. The size of this antenna unit is reduced to the point where internal noise is comparable to external to achieve maximum compactness. High sensitivity is achieved with an efficient class of pulsed/gated, linearly swept-frequency waveforms that are generated and processed digitally. For backscatter radars, close to 50% duty factors are realized. The rules for waveform design and processing overcome problems of range/Doppler aliasing and/or blind zones. After mixing in the receiver, processing bandwidths are much less than RF signal bandwidths, so that simple, inexpensive personal computers are used for real-time signal processing. Digital FFT algorithms determine target range and Doppler, and DF algorithms determine its angles. Frequency hopping can be incorporated in the waveform design by synchronizing all timing and sampling functions, allowing spread-spectrum advantages while still achieving the high sensitivity afforded by coherent processing.

Claims

1. A compact antenna for reception of radar signals, the antenna being part of a radar signal receiving system which includes a receiver and a transmission line, the antenna having an electrical efficiency which is a function of frequency and which causes an external source to contribute an external noise signal during detection of a desired signal, the antenna comprising:

two magnetic dipoles with each dipole having a phase center, the magnetic dipoles being contained in orthogonal planes and having co-linear phase centers; and

an electric dipole having a phase center, the electric dipole being contained in a plane which is mutually orthogonal to the planes of the magnetic dipoles, the phase center of the electric dipole being co-linear with the phase centers of the magnetic dipoles, wherein the antenna has a desired electrical efficiency which results in the external noise signal being substantially equivalent to but of greater magnitude than an internal noise signal resulting from sources internal to the receiver, transmission line, and antenna.

2. The compact radar antenna of claim 1, further comprising:

a third magnetic dipole having a phase center, wherein the phase centers of the three magnetic dipoles and the electric dipole are co-located.

3. The compact radar antenna of claim 1, wherein the desired efficiency of the antenna is achieved by having:

space="preserve" listing-type="equation">F.sub.E <

F.sub.A,

where

F_e is the amount by which internal noise falls below external noise at the frequency corresponding to the received radar signal and F_A is proportional to the antenna efficiency,

where ##EQU6## R_R is a radiation resistance of the antenna, R_L is a remaining resistance of the antenna, transmission line and/or load, and X_L is a remaining reactance of the antenna and/or load.

4. The compact radar antenna of claim 1, wherein the magnetic dipoles are constructed from multiple turns of wire around a non-permeable core, and further wherein, the total length of the multiple turns of wire is less than one tenth of the wavelength of the received radar signal.

5. The compact radar antenna of claim 1, wherein the magnetic dipoles are constructed from multiple turns of wire around a permeable core, and further wherein, the total length of the multiple turns of wire is less than one tenth of the wavelength of the received radar signal.

6. The compact radar antenna of claim 1, wherein the magnetic dipoles are constructed from capacitor-tuned loopsticks.

7. A method for determining the azimuth angle to an object, the method comprising:

receiving a vertically polarized signal from the object by means of a compact radar antenna, the antenna being part of a radar signal receiving system which includes a receiver and a transmission line, the antenna having an electrical efficiency which is a function of frequency and which causes an external source to contribute an external noise signal during detection of a desired signal, wherein the antenna comprises;

two magnetic dipoles with each dipole having a phase center, the magnetic dipoles being contained in orthogonal planes and having co-linear phase centers;

an electric dipole having a phase center, the electric dipole being contained in a plane which is mutually orthogonal to the planes of the magnetic dipoles, the phase center of the electric dipole being co-linear with the phase centers of the magnetic dipoles, wherein the antenna has a desired electrical efficiency which results in the external noise signal being substantially equivalent to but of greater magnitude than an internal noise signal resulting from sources internal to the receiver, transmission line, and antenna; and

processing the received signal to determine the azimuth angle.

8. The method of claim 7, wherein the processing of the received signal to obtain the azimuth angle comprises the following steps:

(1) measuring the voltages produced on each of the magnetic and electric dipoles upon reception of the vertically polarized signal;

(2) representing the voltage measured on one of the magnetic dipoles as S cos Φ

, the voltage measured on the second magnetic dipole as S sin Φ and

the voltage measured on the electric dipole as S, where S is the complex amplitude of the received signal; and

(3) using the voltages measured on the two magnetic dipoles and the electric dipole to solve for Φ

, where Φ

represents the azimuth angle.

9. The method of claim 7, wherein the desired efficiency of the antenna is achieved by having:

space="preserve" listing-type="equation">F.sub.E <

F.sub.A,

where

F_E is the amount by which internal noise falls below external noise at the frequency corresponding to the received radar signal and F_A is proportional to the antenna efficiency,

where ##EQU7## R_R is a radiation resistance of the antenna, R_L is a remaining resistance of the antenna, transmission line and/or load, and X_L is a remaining reactance of the antenna and/or load.

10. A method for determining the azimuth and elevation angles to an object, the method comprising:

receiving an arbitrarily polarized signal from the object by means of a compact radar antenna, the antenna being part of a radar signal receiving system which includes a receiver and a transmission line, the antenna having an electrical efficiency which is a function of frequency and which causes an external source to contribute an external noise signal during detection of a desired signal, wherein the antenna comprises;

three magnetic dipoles with each dipole having a phase center, the magnetic dipoles being contained in orthogonal planes and including two orthogonal horizontal magnetic dipoles and one mutually orthogonal vertical magnetic dipole; and

an electric dipole having a phase center, wherein the phase centers of the magnetic dipoles and the phase center of the electric dipole are co-located, and further, wherein the antenna has a desired electrical efficiency which results in the external noise signal being substantially equivalent to but of greater magnitude than an internal noise signal resulting from sources internal to the receiver, transmission line, and antenna; and

processing the received signal to determine the azimuth and elevation angles.

11. The method of claim 10, wherein the processing of the received signal to obtain the azimuth and elevation angles comprises the following steps:

(1) measuring the voltages produced on each of the magnetic and electric dipoles upon reception of the arbitrarily polarized signal;

(2) representing the voltage measured on the vertical magnetic dipole as F_h cos μ

, the voltage measured on the electric dipole as F_v cos μ

, the dipoles as F_v cos Φ

+F_h sin μ

sin Φ and

the voltage measured on the other horizontal magnetic dipole as-Fv sin Φ

+F_h sin μ

cos Φ

, where F_v is the field strength of the vertically polarized component of the received signal and F_h is the field strength of the horizontally polarized component of the received signal; and

(3) using the voltages measured on the three magnetic dipoles and the electric dipole to solve for and μ

, where Φ

represents the azimuth angle and μ

represents the elevation angle.

12. The method of claim 10, wherein the desired efficiency of the antenna is achieved by having:

space="preserve" listing-type="equation">F.sub.E <

F.sub.A,

where

F_E is the amount by which internal noise falls below external noise at the frequency corresponding to the received radar signal and F_A is proportional to the antenna efficiency,

where ##EQU8## R_R is a radiation resistance of the antenna, R_L is a remaining resistance of the antenna, transmission line and/or load, and X_L is a remaining reactance of the antenna and/or load.

13. A method of generating a radar waveform and processing a received radar signal which is the result of the waveform being reflected by an object to obtain direction, range, and doppler or radial velocity data for the object, the method comprising:

(1) generating a waveform having a substantially linear increase in frequency during a sweep repetition time interval, the waveform having a sweep width or increase in frequency dependent upon a desired range resolution, wherein the waveform is repeated during each subsequent sweep repetition time interval, the sweep repetition interval being equal to the reciprocal of a sweep repetition frequency;

(2) transmitting the waveform by an antenna which is connected to a transmitter operating in a pulsed mode, wherein the pulse period is less than the sweep repetition interval, and further, wherein the transmitter is operated so that it has a duty factor of up to fifty percent;

(3) receiving the reflected waveform with an antenna which is connected to a receiver, the receiver being gated so that it is turned off during the transmission of the waveform by the transmitter;

(4) mixing the received waveform with the waveform generated in (1), thereby producing a baseband radar echo signal having a center near zero frequency, the radar echo having an offset from zero frequency which depends on a range to the object and the object'"'"'s radial velocity;

(5) sampling the mixed waveform at a sampling rate which is less than a signal bandwidth corresponding to a desired target range resolution, wherein the sampling rate is higher than two times a bandwidth of a modulation of the mixed waveform corresponding to data which is the target signal information; and

(6) processing the sampled waveform to obtain range, doppler, and directional information for the object.

14. The method of claim 13, wherein the processing of the sampled waveform further comprises:

(1) performing a first Fast-Fourier-Transform on the sampled data to obtain the range of the object; and

(2) performing a second Fast-Fourier-Transform on a subset of the data obtained from performing the first Fast-Fourier-Transform of the sampled data to obtain the doppler or radial velocity of the target.

15. The method of claim 13, wherein the sweep width, B, is related to the desired range resolution, Δ

R, by

space="preserve" listing-type="equation">B=c/(2Δ

R),

where c is equal to the speed of light.

16. The method of claim 13, wherein the sweep repetition frequency, SRF, is substantially equal to twice a maximum doppler value expected for the object reflecting the transmitted waveform, the maximum doppler value being equal to

17. The method of claim 13, wherein the pulsing of the transmitter and gating of the receiver are performed in a manner so that a first spectral sideband at the pulse repetition frequency is greater in magnitude than a baseband information signal of all possible received object signals, thereby providing a method of generating a radar waveform and processing a received radar signal which significantly reduces range aliasing.

18. The method of claim 13 wherein the processing of the sampled waveform further comprises:

sampling the previously sampled waveform to produce a time series of data, the sampling being performed at a sampling rate equal to M times the pulse repetition frequency, wherein M is a power of two;

segmenting the time series into M separate sub-series, wherein each sub-series has a length substantially equal to 1/M of the unsegmented time series, and further wherein, each sub-series consists of every M-th consecutive point of the unsegmented time series;

performing a first Fast-Fourier-Transform on each of the M separate sub-series to obtain the range of the object;

performing a second Fast-Fourier-Transform on the data obtained from performing the first Fast-Fourier-Transform on each of the M separate sub-series to obtain the doppler or radial velocity of the target; and

recombining the data obtained from performing the second Fast-Fourier-Transform on each of the M separate sub-series into a single series, thereby significantly reducing range or doppler aliasing when the pulsing of the transmitter and gating of the receiver cannot be repeated at a rate so that a first spectral sideband at the pulse repetition frequency is greater in magnitude than a baseband information signal of all possible received object signals.

19. The method of claim 13, wherein the receiving antenna further comprises:

two magnetic dipoles with each dipole having a phase center, the magnetic dipoles being contained in orthogonal planes and having co-linear phase centers; and

an electric dipole having a phase center, the electric dipole being contained in a plane which is mutually orthogonal to the planes of the magnetic dipoles, the phase center of the electric dipole being co-linear with the phase centers of the magnetic dipoles, wherein the antenna has a desired electrical efficiency which results in an external noise signal being substantially equivalent to but of greater magnitude than an internal noise signal.

20. The method of claim 19, wherein the desired efficiency of the antenna is achieved by having:

space="preserve" listing-type="equation">F.sub.E <

F.sub.A,

where

F_E is the amount by which internal noise falls below external noise at the frequency corresponding to the received radar signal and F_A is proportional to the antenna efficiency,

where ##EQU9## where, R_R is a radiation resistance of the antenna, R_L is a remaining resistance of the antenna, transmission line and/or load, and X_L is a remaining reactance of the antenna and/or load.

21. The method of claim 13, wherein the receiving antenna further comprises:

three magnetic dipoles with each dipole having a phase center, the magnetic dipoles being contained in orthogonal planes and including two orthogonal horizontal magnetic dipoles and one mutually orthogonal vertical magnetic dipole; and

an electric dipole having a phase center, wherein the phase centers of the magnetic dipoles and the phase center of the electric dipole are co-located, and further, wherein the antenna has a desired electrical efficiency which results in the external noise signal being substantially equivalent to but of greater magnitude than an internal noise signal.

22. The method of claim 21, wherein the desired efficiency of the antenna is achieved by having:

space="preserve" listing-type="equation">F.sub.E <

F.sub.A,

where

F_E is the amount by which internal noise falls below external noise at the frequency corresponding to the received radar signal and F_A is proportional to the antenna efficiency,

where ##EQU10## where, R_R is a radiation resistance of the antenna, R_L is a remaining resistance of the antenna, transmission line and/or load, and X_L is a remaining reactance of the antenna and/or load.

23. The method of claim 19, wherein the processing of the sampled waveform to obtain the directional information to the object further comprises:

(1) measuring the voltages produced on each of the magnetic and electric dipoles upon reception of a vertically polarized signal;

(2) representing the voltage measured on one of the magnetic dipoles as S cos Φ

, the voltage measured on the second magnetic dipole as S sin Φ and

the voltage measured on the electric dipole as S, where S is the complex amplitude of the received signal; and

(3) using the voltages measured on the two magnetic dipoles and the electric dipole to solve for Φ

, where Φ

represents the azimuth angle.

24. The method of claim 21, wherein the processing of the sampled waveform to obtain the directional information to the object further comprises:

(1) measuring the voltages produced on each of the magnetic and electric dipoles upon reception of an arbitrarily polarized signal;

(2) representing the voltage measured on the vertical magnetic dipole as F_h cos μ

, the voltage measured on the electric dipole as F_v cos μ

, the voltage measured on one of the horizontal magnetic dipoles as F_v cos Φ

+F_h sin μ

sin Φ and

the voltage measured on the other horizontal magnetic dipole as-Fv sin Φ

+F_h sin μ

cos Φ

, where F_v is the field strength of the vertically polarized component of the received signal and F_h is the field strength of the horizontally polarized component of the received signal; and

(3) using the voltages measured on the three magnetic dipoles and the electric dipole to solve for Φ and

μ

, where Φ

represents the azimuth angle and μ

represents the elevation angle.

25. The method of claim 13, wherein the generated waveform further comprises:

a substantially linear decrease in frequency during the sweep repetition time interval, the linear decrease being performed consecutive to the linear increase in frequency, wherein the linear increase and decrease in frequency have the same sweep width.

26. The method of claim 25, wherein the processing of the sampled waveform further comprises:

performing a Fast-Fourier-Transform on the sampled data to obtain the range and doppler or radial velocity of the object.