Gyro Flashcards

1
Q

Drift

A

Rotation in horizhontal direction

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2
Q

Rigidity

A

Maintains its orientation in space
(Second law of newton)

Requirments:
~dense material
~outer rim which increase radius
~high rotational speed ,RPM 15000 to 25000

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3
Q

Precession

A

The force applied is been applied 90 degrees further the gyro rotor

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4
Q

Gimbals

A

The mounting system comprises bearing and supporting frames collectively known as Gimbals

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5
Q

Vertical gyro
Horizhontal gyro

A

Vertical : when the axes is in vertical
Horizontal : when the axes is horizonthal

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6
Q
A

2 degress of freedom wiht two gimbals
The spin axes is never counted as degree of freedom

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7
Q

Rate of gyro

A

Rate gyro when the gyro has one degree of freedom (one gimbal)

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8
Q

Space gyro

A

When it has 2 degrees of freedom ( 2 gimbals)

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9
Q

Directional gyro

A

2 gimbals

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10
Q

Attitude indicator

A

2 degrees

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11
Q

Turn indicator

A

1 gimnbal and spring

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12
Q

Wander summary

A

~Wander : topple, drift

~real/random wander: mechanical imperfections, latitude nut

Apparent wander:earth, transport wander

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13
Q
A

All gyros suffer from real wonder (mechanical imperfection)

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14
Q

ERECTION SYSTEMS

A

To cope with topple we need an errection system

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15
Q
A

Earth rotion 600kts
15.04 degree per hour

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16
Q

Earth rate

A

Varies with latitude for directional gyro
15.04 x sine lat

17
Q

Vertical gyro
Like in the equator

A

No drift ,max topple

18
Q

Horizontal.
Like in the poles

A

Max drift ,no topple

19
Q

Apparetn topple /drift

A

At the pole

~vertical gyro appear not to drift or topple
~horizontal gyro appear to drift

At the equator
~vertical gyro appear to topple
~an east aligned horizontal gyro appears to topple backwards to the vertical
~a north aligned horizontal gyrp will not topple or drift if it remains on th equator

20
Q

Real wander

A

~Random wander: due to mechanical imperfection
~latitude compesation :(gimbal input) influence by gravity erection system

21
Q

Horizontally tied

A
22
Q

Latitude nut

A

Operational latitude ,small nut is adjusted on the gryo’s spin axis which inputs a real wander effect to correct its positon using the principle precession

23
Q

Vetical tied

A

To keep the instrument gry ospin axis vertically tied a sub system causes a deliberate wander effect

24
Q

Principle of precession

A

Precession used to correct for apperent wander (earth rate drift) in the direcrion gyro

25
Q

The pirnciple of precession is used

A

For correct apparent wander ( topple) in the attitude indicator

26
Q

Pneumatic driven

A

The air in requires filtering
Vacuum gauge indicates vacuum pressure

27
Q

Electrically dirven

A

Advantages :
~higher rpms
~more accurate
~more reliable

~DC power supplying a DC motor
~Dc power to an inverter to supply constant frequency ac from an acmotor
~contanstan frequecny ac power to drive an ac motor
~frequency wild CANNOT be directly used

28
Q

Electrically driven

A

Micro electro mechanical sesnors
~ring laser
~smaller lighter
~more reliable
~more accurate
~chea[er to purchase and maintain

29
Q

Redundancy

A

Light a/c will have
Air driven pump for AI and DI ,and electrically driven for the turn indicator ,if the generators fails the turn coordinator will be still powered until battery dies