nauman said:
Details of radio receiver are not known but this is the device which demodulates and provide 155 Hz audio signal to motor as feedback.
The AN/ANA-50 DFG switches at between 75 and 200 Hz. How do you know it uses only a 155 Hz lobing clock? I believe the master two phase lobing clock is generated by that unidentified receiver to control the antenna lobing switch. The returned audio is then synchronously detected by the unidentified receiver block, which controls the antenna 115V 400 Hz motor drive, which has the synchro to send the heading relative direction to the two cockpit display instruments.
The receiver block also contains a T/R switch for voice communication over the VHF/UHF channel using a separate TX antenna on the aircraft. The frequency control, RX mode, and press to talk mic is in the cockpit with the DF display, integrated into the pilot and 1st officer instruments.
To use the antenna alone;
1. You will need to generate the lobing clock to switch the antenna. Maybe 28 Vdc ?
2. You then need a receiver for the 225 to 400 MHz RF, that will produce the audio.
3. A synchronous detector, with an amplifier to drive the 115 V, 400 Hz antenna motor.
4. Some way of converting the antenna synchro signal into a direction display.
5. A vehicle like an aircraft that can support the antenna and provide power.
6. A test signal in the RF band that you need to DF, that might justify the exercise.
The antenna is just one part of a complex integrated group of modules in the avionics area and the cockpit. The last design specifications (including the power wiring connectors) for the AN/ANA-50 DFG were defined in MIL-D-38402A(USAF) 23 APR 87.