TCAS bearing estimation receiver using a 4 element antenna

• US 4,855,748 A
• Filed: 03/18/1988
• Issued: 08/08/1989
• Est. Priority Date: 03/18/1988
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Alliedsignal Inc.
• Inventors: Kyriakos, Constantinos S., Spires, Randall C., Jugs, Andrejs, Brandao, Ruy L.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US07/170,227
• Time in Patent Office: 508 Days
• Field of Search: 342/455, 342/374, 342/420, 342/442, 364/461
• US Class Current: 342/455
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft

Abstract

A direction finding receiving system for use on a protected aircraft in which a signal from an ATCRABS transponder on an intruder aircraft is received has been described incorporating a four element interferometer type antenna array, reversing switches, individual receivers, a phase detector and a processor for processing the outputs of the phase detector. The invention overcomes the problem of correcting for the difference in phase delay of signals passing through the receivers.

Claims

1. A direction finding antenna system for determining the relative bearing of an intruder aircraft from a protected aircraft in conjunction with a Traffic Alert Collision Avoidance System (TCAS), the intruder aircraft being equipped to transmit signals received by said antenna system, comprising

first and third spaced apart antennas mounted aboard the protected aircraft;

first and third receivers aboard the protected aircraft for amplifying, converting and limiting the signals received by said first and third antennas;

first switching means at the inputs to said first and third receivers for interchangeably applying the signals received by said first and third antennas to the inputs of said first and third receivers;

second switching means at the outputs of said first and third receivers;

a first phase detector having a reference phase input and a variable phase input,

said inputs to said first phase detector being connected to said second switching means,

said second switching means operating in synchronism with said first switching means so that in a first position of said first switching means signals from said first and third antennas are applied to said first and third receivers, respectively, and in a first position of said second switching means the outputs of said first and third receivers are applied respectively to said reference phase and said variable phase inputs to said first phase detector and in a second position said first switching means signals from said first and third antennas are applied to the inputs of said third and first receivers, respectively, in a second position of second switching means the outputs of said third receiver and said first receiver are applied respectively to said reference phase and variable phase inputs to said first phase detector; and

first means for processing the outputs of said first phase detector obtained in alternate operations of said first and second switching means to eliminate the errors therein caused by a difference between the phase delays of signals passing through said first and third receivers, the result of said processing means being a first quantity related to the relative bearing to the intruder aircraft from the protected aircraft.

2. An antenna system as claimed in claim 1, with additionally;

second and fourth antennas mounted aboard the protected aircraft, said first, second, third and fourth antennas being mounted in cruciform configuration;

second and fourth receivers aboard the protected aircraft for amplifying, convering and limiting the signals received by said second and fourth antennas;

third switching means at the inputs to said second and fourth receivers for interchangeably applying the signals received by said second and fourth antennas to the inputs of said second and fourth receivers;

fourth switching means at the outputs of said second and fourth receivers;

a second phase detector having a reference phase input and a variable phase input,

said inputs to said second phase detector being connected to said fourth switching means,

said fourth switching means operating in synchronism with said third switching means so that in a first position of said third switching means signals from said second and fourth antennas are applied to said second and fourth receivers, respectively, and in a first position of said fourth switching means the outputs from said second and fourth receivers respectively are applied to said variable phase and said reference phase inputs to said second phase detector and in a second position of said third switching means signals from said second and fourth antennas are applied to said fourth and second receivers, respectively, and in a second position of said fourth switching means the outputs from said second and fourth receivers are applied, respectively, to said variable phase and said reference phase inputs to said second phase detector; and

second means for processing the outputs of said second phase detector obtained in alternate operations of said third and fourth switching means to eliminate errors therein caused by a difference between the phase delays of signals passing through said second and fourth receivers, the result of said second processing means being a second quantity related to the relative bearing to the intruder aircraft from the protected aircraft.

3. An antenna system as claimed in claim 2, with additionally,

third means for processing the results of said first and second processing means to obtain the relative bearing angle to the intruder aircraft from the protected aircraft.

4. An antenna system as claimed in claim 1, with additionally:

first means for determining errors in said ouputs of said first phase detector due to non-linear operation of said first phase detector; and

first means for correcting said outputs of said first phase detector in accordance with the errors therein determined by said last named first means.

5. An antenna system as claimed in claim 2, wth additionally:

second means for determining errors in said outputs of said second phase detector due to non-linear operation of said second phase detector; and

second means for correcting said outputs of said second phase detector in accordance with the errors therein determined by said last named second means.

6. An antenna system as claimed in claim 1 wherein:

the output of said first phase detector is identified as Phase AB when said first and second switching means are in their said first positions; and

the output of said first phase detector is identified as Phase BA when said first and second switching means are in their second positions; and

wherein said means for processing the outputs of said first phase detector includes means for solving the algorithm;

space="preserve" listing-type="equation">First Actual Phase =(Phase AB+Phase BA) 2,

said First Actual Phase being said first quantity.

7. An antenna system as claimed in claim 2 wherein:

the output of said second phase detector is identified as Phase CD when said third and fourth switching meas are in their said first positions; and

the output of said second phase detector is identified as Phase DC when said third and fourth switching means are in their second positons; and

wherein said means for processing the outputs of said second phase detector includes means for solving the algorithm;

space="preserve" listing-type="equation">Second Actual Base=(Phase CD+Phase DC) 2,

said Second Acual Phase =(Phase CD+Phase DC) 2

Said Second Actual Phase being said second quantity.

8. antenna system as claimed in claim 7, with additionally:

third means for processing said First Actual Phase and said Second Actual Phase to obtain the relative bearing to the intruder aircraft from the protected aircraft.

9. An antenna system as claimed in claim 1, wherein:

said first and third antennas are connected to said first shitching means by first and third transmission lines; and

with additionlly,

first means for determining the difference between the phase delays of signals passing through said first and third transmission lines; and

means for correcting said outputs of said first phase detector in accordance with said difference determined by said last named first means.

10. An antenna system as claimed in claim 2, wherein:

said second and fourth antennas are conected to said third switching means by second and fourth transmission lines; and

with additionally,

second means for determining the difference between the phase delays of signals passing through said second and fourth tranmission lines; and

means for correcting said outputs of said second phase detector in accordance with said diffence determined by said last named second means.

11. An antenna system as claimed in claim 9 wherein:

said first means for determining the difference between the phase delays of signals passing through said first and second transmission lines includes;

a test oscillator; and

first means for radiating isophase signals from said thest oscillator for reception by said first and third antennas.

12. An antenna system as claimed in claim 10 wherein:

said second means for dermining the difference between the phase delays of signals passing through said second and fourth transmission lines includes;

a test oscillator; and

second means for radiating isophase signals from said test oscillator for reception by said second and fourth antennas.

13. An antenna system as claimed in claim 12, wherein:

there is but a single test oscillator, and

said first means for radiating signals from said test oscillator includes means for applying signals from said single test oscillator to said second antenna for radiation; and

wherein

said second means for radiating signals from said test oscillator includes means for applying signals from said single test oscillator to said second antenna for radiation.

14. An antenna system as claimed in claim 4, wherein:

said first means for determining errors in said outputs of said first phase detector includes;

means for applying a first alternating test voltage to said reference phase input of said first phase detector;

means for applying a second alternating test voltage to said variable phase input of said first phase detector, said second test voltage having a phase relationship to said first test voltage which varies linearly with time; and

first means for periodically sampling the output of said first phase detector to provide a first sequence of output data samples which are equally spaced in time.

15. An antenna system as claimed in claim 5, wherein:

said second means for determining errors in said outputs of said second phase detector includes;

means for applying a third alternating test voltage to said reference phase input of said second phase detector;

means for applying a fourth alternating test voltage to the variable phase input of said second phase detector, said fourth test voltage having a phase relationship to said third test voltage which varies linearly with time; and

second means for periodically sampling the output of said second phase detector to provide a second sequence of output data samples which are equally spaced in time.

16. An antenna system as claimed in claim 14 wherein:

said first test voltage is derived from a first table oscillator operating at a first frequency; and

said second test voltage is derived from a second stable oscillator operating a second frequency different from said first frequency.