Heading Indicator | Gyromagnetic Compass Flashcards

1
Q

A DRC’s indications get ___ nearer to the Poles

A

weaker

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2
Q

A gyrocompass is a DGI that ___

A

aligns itself

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3
Q

In an area with ___ magnetic flux, such as the Poles, you should disable the automatic slaving and use the instrument as a DGI

A

weak

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4
Q

The gyroscope provides short term stability for the ___ reference

A

azimuth

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5
Q

The gyroscope has _ degrees of freedom, and the input axis is ___, meaning that the spin axis is ___

A

2 vertical horizontal

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6
Q

The erection mechanism keeps the axis ___

A

horizontal

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7
Q

The flux valve detects the element of the ____

A

Earth’s mag field

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8
Q

The flux valve should be positioned ___

A

as far as possible from magnetic influence

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9
Q

If the flux valve ceases to provide reliable information, it may generate a red ___ message on the ___

A

HDG HDI

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10
Q

The flux valve will provide a torque on the ___ axis

A

sensitive

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11
Q

The flux valve works on the principle that You can produce your own flux which changes with _, then measure that and interpret the resulting ___

A

H, voltage

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12
Q

The measuring of flux is done with a device which has _ transformers, at ___ degrees to each other, with a curved horn at their ends to maximise reception

A

3 120

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13
Q

_ spokes allow the flux valve’s orientation to the North

A

3

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14
Q

Flux valves are made of ___ as it loses magnetic influence once the power is gone, and can be magnetised quickly.

A

permalloy

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15
Q

Hysteresis is the property of ___

A

being able to lose magnetic influence once power is removed

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16
Q

The ___ influence is obtained when the spoke is in line with the Earth’s magnetic field, and any in between vary with the ___ of the Magnetic Heading

A

maximum cosine

17
Q

An exciter coil is placed in the centre, and fed with ___ Hz single phase _C to allow a reversing magnetic field to be created through the primary coil around each spoke.

A

400 A

18
Q

With the aircraft on a fixed heading, the field remains ___

A

constant

19
Q

When the aircraft turns, the magnetic field changes and a ___ is induced in the secondary coil

A

current

20
Q

When the AC is pumped through a flux valve, it produces a ripple at twice the frequency of the original current, producing a sinusoidal wave of ___ Hz with the amplitude in proportion with the Earth’s magnetic field, and the ___ of the magnetic heading.

A

800 cosine

21
Q

It is suspended in a hooke’s joint to capture as much _ as possible, rather than _, which is responsible for turning errors

A

H z

22
Q

The system ___, rather than seeks

A

senses

23
Q

The information from the flux valve is compared to what the display says, and the results are sent to an ___ ___. The signals are passed through ___ and ___ ___, which precesses the directional gyro

A

error detector, amplifier, torque motor

FEAT

24
Q

The current flows through the ___, which tells you that synchronisation is taking place correctly.

A

annunciator

25
Q

The synchronisation knob is there for manual correction of gross ___ in level flight; it has the same function as the caging knob

A

topple

26
Q

___ error arises from banking, and disappear once the turn is complete

A

gimballing

27
Q

___ accelerations which make the flux valve tilt can cause heading errors.

A

Horizontal

28
Q

A ___ rate of turn in a ___ aircraft would show the greatest heading error

A

high, fast

29
Q

Slow prolonged turns at high speeds generate the ___ errors

A

greatest

30
Q

Coriolis error can (not) be calculated and compensated for

A

it can

31
Q

Whenever you fly a rhumb line, the aircraft must turn to maintain a constant track, which is an acceleration that displaces the detector from the ___ plane. This is ___ Error

A

horizontal, Vehicle Movement

32
Q

Vibrations can result in heading ____

A

oscillation

33
Q

The ___ is the mechanism by which information is sent to the crew stations and instruments

A

Transmission Display System

34
Q

The torque motor makes the gyro precess in azimuth at about _ degrees per minute

A

2

35
Q

A ___ shows when it’s being precessed in one direction, a ___ in another

A

dot, cross

36
Q

In normal ops, the dot and cross should oscillate ___

A

quickly

37
Q

The most significant errors are ___

A
  • Apparent and real wnder
  • Gimballing
  • Mech defects
  • Low rotor speed
38
Q

Outline how the error detector works

A

It compares the data from the flux valve with the indication of the gyromagnetic compass.