Hybrid amplitude/phase comparison direction finding system

• US 5,541,608 A
• Filed: 03/29/1995
• Issued: 07/30/1996
• Est. Priority Date: 03/29/1995
• Status: Expired due to Term

• Current Assignee: Exelis Incorporated (L3Harris Technologies, Inc.)
• Original Assignee: ITT Corporation (ITT, Inc.)
• Inventors: Harding, Albert C., Menegozzi, Lionel N., Murphy, Myles P.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US08/412,461
• Time in Patent Office: 489 Days
• Field of Search: 342/442, 342/432, 342/174
• US Class Current: 342/442
• CPC Class Codes: G01S 3/023 Monitoring or calibrating
• CPC Class Codes: G01S 3/46 using antennas spaced apart and measuring phase or time difference between signals therefrom, i.e. path-difference systems

Abstract

A hybrid amplitude/phase comparison direction finding system for aircraft, employing a unique calibration system to compensate for tolerance variations in the antennas. The calibration system utilizes a programmable read only memory (PROM) for each antenna pair, wherein calibration data from pre-measured antenna patterns of the associated antennas are stored. The calibration data preferably includes measured relative amplitude (electromagnetic field strength) and phase data, as a function of frequency and angle from a common reference plane, for the associated antenna pair. This calibration data is stored in a PROM which is preferably disposed within an assembly which includes the antenna pair. A system processor can then retrieve the calibration data during system operation, whereupon angle of arrival measurements can be performed with improved accuracy.

Claims

1. A system for measuring an angular position of an aircraft with respect to a reference ground location, comprising:

a pair of antennas disposed at said ground location with each antenna of said pair having an antenna beam pointing in a different direction from the other and independently receiving electromagnetic energy propagating from the aircraft'"'"'s position;

an electronic memory having stored calibration data corresponding to premeasured amplitude and phase radiation patterns of said antennas, as a function of frequency and angle from a common reference plane;

receiving means, coupled to said antenna pair, for converting said electromagnetic energy independently received by said antennas to a lower frequency, and for detecting the frequency of said propagating electromagnetic energy to provide a measured frequency value;

means coupled to said receiving means, for comparing the amplitude and phase of said electromagnetic energy independently received by said antennas wherein a relative amplitude value and a relative phase value are provided; and

processing means, coupled to said receiving means, said means for comparing, and to said memory, for determining the angular position of said aircraft from said measured frequency value, said relative amplitude value, said relative phase value and said calibration data.

2. The system according to claim 1, wherein said pair of antennas and said electronic memory are disposed within an antenna assembly independent of said processing means.

3. The system according to claim 2 wherein said electronic memory comprises a programmable read only memory (PROM).

4. The system according to claim 3 wherein said pair of antennas comprise a pair of broad beam spiral antennas of generally the same dimensions in a fixed relationship to one another, and wherein said PROM is disposed in a housing affixed to said pair of antennas.

5. The system according to claim 4, wherein said pair of antennas are affixed to one another by means of a frame member defining a central boresight axis and wherein each of said antennas have apertures squinted from said central boresight axis by a given squint angle.

6. The system according to claim 1 wherein said stored calibration data includes a table of frequencies, a table of said angle from a common reference plane corresponding to each of said frequencies and ranging from a first angular extreme to a second angular extreme, a table of measured relative amplitude data points between said pair of antennas at each of said angles and frequencies, and a table of measured relative phase data points between said pair of antennas at each of said angles and frequencies.

7. The system according to claim 6 wherein said processing means determines said angular position by matching said measured frequency with one of said frequencies stored in said table of frequencies, matching said relative phase value with at least one of said relative phase data points corresponding to said one of said frequencies, and matching said relative amplitude value with one of said relative amplitude data points corresponding to said at least one of said relative phase data points, and retrieving the angle corresponding to said relative amplitude data point matching said relative amplitude value.

8. The system according to claim 1 further including a first transmission line of a given electrical length having a first end coupled to one of said pair of antennas and a second end coupled to a first input port of said receiving means, and a second transmission line of said given electrical length having a first end coupled to the other of said pair of antennas and a second end coupled to a second input port of said receiver means, and wherein said calibration data corresponds to pre-measured amplitude and phase radiation patterns of said antennas measured to said second end of each of said transmission lines.

9. The system according to claim 8 wherein said receiver means comprises first and second mixers coupled to said input ports, a local oscillator coupled to each of said mixers, a pair of intermediate frequency (IF) amplifiers coupled to said mixers, a pair of filters coupled to said IF amplifiers, and a frequency discriminator coupled to said filters;

and

wherein said means for comparing comprises a phase comparator coupled to said filters for providing said relative phase value, and a software routine within said processing means for determining said relative amplitude value from a pair of measured amplitude values supplied thereto, each of said measured amplitude values being indicative of electromagnetic field strength of energy received by an associated one of said pair of antennas.

10. The system according to claim 9 further comprising log amplication means coupled to said filters and threshold detection means coupled to said log amplification means.

11. The system according to claim 10 further including an analog to digital (A/D) converter coupled between said threshold detection means and said processing means and between said phase comparator and said processing means, said A/D converter converting a phase comparison value of said phase comparator to a first digital word indicative of said relative phase value, and converting a pair of output signals from said threshold detection means to a pair of digital words, said pair of digital words being indicative of said measured amplitude values.

12. The system according to claim 1 wherein said pair of antennas have broad antenna beams pointing at different azimuth directions to enable azimuth angular positions of aircraft to be measured over an azimuthal field of view of at least 90 degrees.

16. The system according to claim 12 further including means coupled to said antennas and to said processing means for converting said electromagnetic energy independently received to digital words each indicative of a characteristic of the electromagnetic energy received by one of said antennas;

and

wherein said processing means includes said means for providing said one comparison parameter, said processing means comparing said digital words to determine said comparison parameter.

13. A system for measuring an angular direction of incoming electromagnetic energy, comprising:

an antenna assembly including at least two antennas for independently receiving the incoming electromagnetic energy, and an electronic memory having stored calibration data indicative of pre-measured radiation pattern characteristics of said antennas;

means coupled to said antennas for providing a frequency measurement of the incoming electromagnetic energy;

means coupled to said antennas for providing comparison parameters indicative of a difference between the electromagnetic energy independently received by said antennas, wherein said comparison parameters include a relative phase value and a relative amplitude value of the electromagnetic energy independently received by said antennas;

processing means, separate from said antenna assembly and coupled to said electronic memory, for retrieving said calibration data and determining said angular direction from said comparison parameters, said frequency measurement and said calibration data.

14. The system according to claim 13, further comprising means coupled to said pair of antennas and to said processing means for measuring the frequency of the electromagnetic energy received and wherein said processing means uses the measured frequency as a parameter in said determination of said angular direction.

15. The system according to claim 13 wherein said antennas have antenna beams pointing in different directions from the other.

17. A method of measuring an angular direction of incoming electromagnetic energy, comprising:

providing at least two antennas disposed in a fixed relationship to one another;

measuring radiation patterns of said antennas, said radiation patterns including both phase patterns and amplitude patterns as a function of frequency and angle from a common reference plane of said antennas;

storing data indicative of said radiation patterns in an electronic memory;

independently receiving said incoming electromagnetic energy with each of said antennas;

detecting the frequency of the electromagnetic energy independently received by said antennas;

comparing the phase of the electromagnetic energy independently received by said two antennas to provide a relative phase value;

comparing the amplitude of the electromagnetic energy independently received by said two antennas to provide a relative amplitude value;

determining said angular direction from said frequency detected, said relative phase value, said relative amplitude value and said data in said electronic memory.

18. The method according to claim 17 wherein said radiation patterns comprise both relative phase and relative amplitude between radiated energy independently received by said two antennas as a function of frequency and angle from a common reference plane of said antennas.

19. The method according to claim 17 wherein said step of determining said angular direction comprises comparing said frequency detected, said relative amplitude value and said relative phase value with said stored data in said electronic memory to retrieve an angle value from said stored data corresponding to said frequency detected, said relative amplitude value and said relative phase value, whereby said angle value represents a measurement of said angular direction of the incoming electromagnetic energy free of ambiguities.

20. The method according to claim 17 wherein said data indicative of said radiation patterns includes a table of a computed distance between phase centers of said two antennas as a function of frequency and angle from a common reference plane, a table of relative amplitude slope as a function of frequency, said relative amplitude slope representing an incremental change in relative amplitude between said two antennas divided by an incremental change in said angle from a common reference plane, and

wherein said step of determining said angular direction comprises retrieving one of said relative amplitude slope values from said electronic memory corresponding to said frequency detected;

computing a coarse angle of arrival from said retrieved amplitude slope value;

retrieving one of said distances between phase centers corresponding to said coarse angle of arrival from said data in said electronic memory;

computing at least one fine angle of arrival from said frequency detected, said relative phase value and said distance between phase centers retrieved from said electronic memory; and

determining a final measured angle of arrival by comparing said at least one of said fine angles of arrival with said coarse angle of arrival to resolve ambiguities in said angular direction.