ADF Receiver Flashcards

1
Q

What is the design of the ADF receiver and its tuning accuracy

A

Superhet receiver with AM detection tuned in 0.5/1.0 kHz Steps with accuracy better than +-175 Hz

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2
Q

What is the loop RF signal and its initial processing?

A

It’s voltage from the Goniometer rotor, amplified, phase shift by 90, its phase relative to the sense RF is key.

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3
Q

How does the balanced modulator affect the loop RF signal?

A

It switches the loop signal at 47~200 Hz alternating it to be in phase or 180 out of phase with the sense RF signal

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4
Q

What occurs when the switched loop RF signal combines with the sense RF signal

A

In the sense amplifier, they add or subtract during each servo oscillator half-cycle, indicating the station’s position

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5
Q

How is the combined RF signal processed before driving the motor?

A

It’s amplified, AM detected (using a diode), then the output is sine-wave shaped by a servo amplifier.

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6
Q

What is the role of the two-phase motor in the ADF system?

A

It rotates the goniometer rotor toward the null position based on the phase difference between its two inputs.

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7
Q

How is the motor’s rotation direction determined?

A

A 90 phase difference drives rotation; a 180 shift reverses it (ACW for left, CW for right)

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8
Q

When does the two phase motor stops?

A

When the goniometer rotor reaches the null (right angle to the magnetic field) , causing the loop RF signal to vanish.

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9
Q

How is the goniometer’s position used for bearing indication?

A

In light aircraft, it drives RBI pointer; in transport aircraft, it couples via a synchro transmitter to an RMI.

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10
Q

What is a relative bearing in this context

A

Bearing of the station measured clockwise from the aircraft’s nose

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11
Q

How is goniometer angular position transmitted remotely?

A

Through a synchro system that mechanically couples the goniometer rotor to a transmitter and receiver.

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12
Q

How does the synchro system indicate a change in relative bearing?

A

An unbalanced synchro induces voltages that drive the bearing indicator pointer pointer to the new position

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13
Q

How does the RMI convert relative bearing to magnetic bearing

A

Its outer compass card is synchronized with the aircraft’s compass system, updating the magnetic heading.

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14
Q

What happens in the CT rotor and servo system when the aircraft heading changes?

A

A proportional error voltage is produced, driving the servo motor to rotate the compass card until the error is zero.

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15
Q

What is the role of the balanced modulator in the ADF receiver?

A

It switches the loop RF signal at 47~200 Hz, alternately making it in phase or 180 out of phase with the sense RF signal.

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16
Q

How does the sense amplifier use the switched loop RF signal?

A

Adds or subtracts it from the constant sense RF signal during each half cycle, based on the goniometer rotor’s position.

17
Q

How is the detector output processed before driving the two phase motor?

A

It is amplified and shaped into a sine wave with a 90 phase shift via servo amplifier.

18
Q

What determines the direction of rotation of the two phase motor?

A

2 phase relationship between the servo oscillator and the detector derived sine wave.

19
Q

How does the system stop the two phase motor?

A

When goniometer motor reaches the null position (no loop RF signal), the detector output drops to zero, halting the motor.

20
Q

What is the purpose of coupling the goniometer to a synchro transmitter in transport aircraft?

A

Remotely display the relative bearing on an RMI via the synchro system.

21
Q

How is the relative bearing defined in this system?

A

Measured clockwise from the aircraft’s nose

22
Q

How is the goniometer search coil adjusted when the aircraft heading changes?

A

It rotates opposite to the heading change to return to the null position, with its angle transmitted by the synchro system.

23
Q

How does the synchro system update the bearing indicator?

A

An unbalanced synchro (due to rotor rotation) induces voltages that rotate the bearing pointer to the new relative bearing.

24
Q

What happens in the CT rotor of the RMI when the aircraft heading is constant?

A

No error voltage is generated, so the compass card remains fixed.

25
Q

How does a change in aircraft heading affect the compass card in the RMI?

A

Produces error voltage in CT rotor, driving servo motor to rotate compass card until the error is nullified, aligning it with the new magnetic heading.