Aircraft proximity sensor system for radio frequency transmission device
An aircraft proximity sensor system includes a control module in communication with a transceiver module and an aircraft proximity sensor module, the control module operable to disable transmission by the transceiver module in response to the aircraft proximity sensor module.
1. An aircraft proximity sensor system, comprising:
a transceiver module;
an aircraft proximity sensor module, said aircraft proximity sensor module includes a tri-axis electromagnet field sensor operable to detect electromagnetic fields generated by an aircraft, and an aircraft/tower radio communication sensor operable to detect transmission on at least one of a Unicom, multicom, Flight Services, and Traffic Advisory (CTAF) frequency for an uncontrolled airport; and
a control module in communication with said transceiver module and said aircraft proximity sensor module, said control module operable to disable transmission by said transceiver module in response to said aircraft proximity sensor module, wherein said control module is operable to disable transmission by said transceiver module in response to said aircraft proximity sensor module being proximate an aircraft with inactive jet engines.
2. The system as recited in claim 1 , wherein said aircraft proximity sensor system is incorporated within a radio frequency transmission device.
3. The system as recited in claim 2 , wherein said radio frequency transmission device includes a data logger.
4. The system as recited in claim 1 , wherein said transceiver module is operable to transmit a cellular signal.
5. The system as recited in claim 1 , wherein said aircraft/tower radio communication sensor is operable to detect transmission between 118.000-136.975 MHz.
6. The system as recited in claim 1 , wherein said aircraft/tower radio communication sensor is operable to detect transmission at 120.000 MHz.
7. The system as recited in claim 1 , wherein said aircraft/tower radio communication sensor is operable to detect transmission on an Air Traffic Control Frequency.
8. The system as recited in claim 1 , wherein said aircraft/tower radio communication sensor is operable to detect transmission on a Company Airlines Operational Control Frequency.
9. The system as recited in claim 1 , wherein said control module is operable to disable transmission by said transceiver module in response to said aircraft proximity sensor module being proximate a stationary aircraft.
10. The system as recited in claim 9 , wherein said tri-axis electromagnet field sensor is operable to detect electromagnetic fields at 400 Hz.
11. A method of transmission control for a data logger, the method comprising:
detecting a proximity to an aircraft via an aircraft proximity sensor module that includes a tri-axis electromagnet field sensor operable to detect electromagnetic fields generated by the aircraft, and an aircraft/tower radio communication sensor operable to detect transmission on at least one of a Unicom, multicom, Flight Services, and Traffic Advisory (CTAF) frequency for an uncontrolled airport; and
disabling transmission from a data logger in response to the proximity with the aircraft while the aircraft has inactive jet engines.
12. The method as recited in claim 11 , wherein detecting the proximity includes detecting the proximity to a stationary aircraft.
13. The method as recited in claim 11 , wherein detecting the proximity includes detecting radio transmission between 118.000- 136.975 MHz.
14. The method as recited in claim 11 , wherein detecting the proximity includes detecting aircraft power system operation.
15. The method as recited in claim 14 , wherein detecting the proximity includes detecting electromagnetic fields generated by the aircraft.
16. The method as recited in claim 14 , wherein detecting the proximity includes detecting electromagnetic fields at 400 Hz.
17. The method as recited in claim 11 , further comprising cycling the detection thereof in a periodic manner to confirm the absence of aircraft/tower radio communication.
18. The method as recited in claim 11 , further comprising cycling the detection continuously to confirm the absence of aircraft/tower radio communication.
19. The method as recited in claim 11 , further comprising enabling transmission from the data logger in response to the proximity subsequent to the disabling.