Aviation transponder

• US 10,705,199 B2
• Filed: 11/30/2017
• Issued: 07/07/2020
• Est. Priority Date: 11/30/2017
• Status: Active Grant

• Current Assignee: Urban Canyon Flight
• Original Assignee: Urban Canyon Flight
• Inventors: Peckham, Canyon Daniel
• Primary Examiner(s): Bythrow, Peter M
• Application Number:
  US15/828,310
• Publication Number:
  US 20190162841A1
• Time in Patent Office: 950 Days
• CPC Class Codes: G01S 1/685 using pulse modulation, e.g. pulse frequency modulation
• CPC Class Codes: G01S 13/765 with exchange of information between interrogator and responder
• CPC Class Codes: G01S 13/767 Responders; Transponders teaching or practice apparatus for gun-aiming or gun-laying using reflecting targets or active targets F41G3/26
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 19/03 Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
• CPC Class Codes: G01S 2205/03 Airborne
• CPC Class Codes: G01S 5/0027 of actual mobile position, i.e. position determined on mobile
• CPC Class Codes: G08G 5/0004 Transmission of traffic-related information to or from an aircraft airborne radio transmission systems in general H04B7/185; airborne wireless networks H04W84/06

Abstract

An improved aviation transponder is discussed herein. The improved aviation transponder demonstrates improved cohabitation and survivability characteristics, allowing the transponder to be placed near other antennas without causing or receiving interference, and reducing potential damage caused by high-energy electromagnetic fields, such as those experienced near an air traffic control (ATC) or military radar installation. Additionally, a small form factor of the transponder results in a smaller, more compact aircraft that consumes less energy, reduces heat dissipation, and maximizes battery life and/or flight time. The transponder may comply with modular interface standards, and may include a radio configured for transmitting 200-watt signals. Based at least in part on the improved performance, the transponder can be implemented in unmanned aerial vehicles (UAVs), for example.

Claims

1. An aviation transponder comprising:

a housing;

at least one antenna port;

at least one input port to receive sensor data;

at least one controller configured to control at least a portion of operations of the aviation transponder;

a local oscillator configured to generate a radio signal at a first frequency;

a distribution component coupled to the local oscillator and configured to selectively couple the local oscillator to a transmit path or a mixer associated with a receive path; and

a switch coupled to an antenna path and configured to selectively couple the antenna path to the transmit path or to the receive path;

wherein the antenna path includes at least one first filter;

wherein the transmit path includes at least one transmit amplifier;

wherein the receive path including at least;

at least one receive amplifier;

at least one second filter; and

the mixer; and

wherein the at least one controller is configured to, at a first time;

enable the at least one transmit amplifier;

cause the switch to couple the transmit path to the antenna path; and

cause the at least one antenna port to output an identification signal.

2. The aviation transponder of claim 1, wherein the aviation transponder supports at least one of:

a Mode A interrogation mode;

a Mode C interrogation mode;

a Mode S interrogation mode;

or

an automatic dependent surveillance broadcast (ADS-B).

3. The aviation transponder of claim 1, wherein the switch is a first switch, and wherein the distribution component is

a second switch.

4. The aviation transponder of claim 1, wherein the switch is a first switch, wherein the distribution component is a second switch, and wherein the controller is further configured to, at a second time:

disable the at least one transmit amplifier;

cause the second switch to couple the local oscillator to the mixer associated with the receive path;

cause the first switch to couple the receive path to the antenna path; and

receive an interrogation signal via the at least one antenna port.

5. The aviation transponder of claim 4, wherein the receive path further includes a Costas loop implemented in hardware, and wherein the Costas loop is configured to determine a phase shift associated with the interrogation signal.

6. The aviation transponder of claim 4, wherein the mixer is configured to:

receive the radio signal from the local oscillator at the first frequency;

receive the interrogation signal at a second frequency; and

determine an intermediate frequency based at least in part on a difference between the radio signal and the interrogation signal.

7. The aviation transponder of claim 1, wherein the local oscillator is implemented as a I/Q modulator configured to support 8 phase shift keying (8PSK).

8. The aviation transponder of claim 1, wherein:

the at least one controller includes a controller and an integrated circuit;

the controller is configured to receive a reference signal from a reference oscillator and to provide the reference signal to the integrated circuit; and

the integrated circuit is configured to receive the reference signal from the controller and to provide the reference signal to the local oscillator.

9. The aviation transponder of claim 1, further comprising an input configured to receive a command to cause the aviation transponder to enter a low power mode.

10. The aviation transponder of claim 1, wherein the at least one transmit amplifier includes at least:

a first transmit amplifier;

a driver amplifier; and

a power amplifier.

11. The aviation transponder of claim 1, wherein the receive path further includes at least one limiter component including:

at least one quarter-wave element, wherein an electrical length of the quarter-wave element is based at least in part on the first frequency; and

at least one diode; and

wherein the at least one quarter-wave element and the at least one diode are configured to direct a signal received via the at least one antenna port to a ground plane at a time in which a power of the signal is above a radio frequency power threshold.

12. The aviation transponder of claim 1, wherein the sensor data includes at least one of:

first sensor data associated with an altitude of an aircraft;

second sensor data associated with a vertical rate-of-change of the aircraft;

third sensor data associated with an airspeed of the aircraft;

heading data associated with a heading of the aircraft;

or

location data associated with the aircraft, the location data based at least in part on a global navigation satellite system (GNSS) signal.

13. A transponder comprising:

at least one antenna port;

at least one controller;

a local oscillator configured to generate a radio signal at a first frequency;

a first switch coupled to the local oscillator and configured to selectively couple the local oscillator to a transmit path or a receive path; and

a second switch coupled to an antenna path and configured to selectively couple the antenna path to the transmit path or to the receive path;

wherein the at least one controller is configured to, at a first time;

cause the first switch to couple the local oscillator to at least a portion of the receive path;

cause the second switch to couple the receive path to the antenna path; and

receive an interrogation signal via the at least one antenna port; and

wherein the at least one controller is configured to, at a second time after the first time;

enable at least one transmit amplifier associated with the transmit path;

cause the first switch to couple the local oscillator to the transmit path;

cause the second switch to couple the transmit path to the antenna path; and

cause the at least one antenna port to output an identification signal at least partially in response to receiving the interrogation signal.

14. The transponder of claim 13, further comprising:

a reference oscillator configured to provide a clock signal to the at least one controller and the local oscillator.

15. The transponder of claim 13, wherein the identification signal is a first identification signal, and wherein the at least one controller is configured to, at a third time:

cause the at least one antenna port to output a second identification signal independent of receiving the interrogation signal.

16. The transponder of claim 13, wherein the transmit path includes at least one transmit amplifier, at least one driver amplifier, and at least one power amplifier.

17. The transponder of claim 13, wherein the receive path further includes a Costas loop implemented in hardware, and wherein the Costas loop is configured to determine a phase shift associated with the interrogation signal.

18. A method comprising:

causing, by at least one controller of a transponder, and at a first time, a first switch to couple a local oscillator to at least a portion of a receive path of the transponder;

causing, by the at least one controller, a second switch to couple the receive path to an antenna path of the transponder;

receiving an interrogation signal via at least one antenna port;

enabling, by the at least one controller, at least one transmit amplifier associated with a transmit path;

causing, by the at least one controller, and at a second time that is different than the first time, the first switch to couple the local oscillator to the transmit path;

causing, by the at least one controller, the second switch to couple the transmit path to the antenna path; and

causing, by the at least one controller, at least one antenna port to output an identification signal at least partially in response to receiving the interrogation signal.

19. The method of claim 18, further comprising:

receiving, by the at least one controller, sensor data from one or more sensors; and

causing, by the at least one controller, a representation of at least a portion of the sensor data to be output along with the identification signal.

20. The method of claim 18, further comprising transmitting the identification signal in accordance with at least one of:

a Mode A interrogation mode;

a Mode C interrogation mode;

a Mode S interrogation mode;

or

an automatic dependent surveillance broadcast (ADS-B).