Chapter 18A - Inertial Navigation Flashcards

1
Q

INS measures?

A

Track and Groundspeed

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2
Q

Is INS self contained?

A

Yes

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3
Q

Any inertial system must be given a _____ on which it will base all its calculations

A
  • starting reference point
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4
Q

INS requires no external information except? and from what?

A

TAS from the ADC

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5
Q

INS follows what?

A

Great Circles

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6
Q

Commonly the alignment of accelerometers is _____ or Longitudinal axis and _____ or Lateral axis.

A
  • North/South
  • East/West
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7
Q

If acceleration is measured, integration with respect to time will provide? Is this first or second stage integration?

A

Velocity

First stage integration

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8
Q

A integration with respect to time will give _____, or distance travelled in a particular direction. Is this first or second stage integration?

A
  • displacement,

Second stage integration

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9
Q

What two things do you need to initially put into an INS?

A

Position, Speed

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10
Q

What navigation capabilities does an INS give you?

A

Position (latitude & longitude)
Heading/drift
Track/groundspeed
Waypoint navigation
Planned track
Distance and time to go
Cross track error
Track angle error

Can also provide:

Roll and Pitch

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11
Q

Accelerometer uses a?

A

Repulsive magnet - bigger the displacement bigger the repulsive force

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12
Q

INS Panels – Mode Select Unit (MSU), STBY is?

A

System powers up, gyros are brought to speed and temperature. The aircraft can be moved.

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13
Q

In EASA you have to be ___ to do an alignment?

A

Stationary

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14
Q

INS Panels – Mode Select Unit (MSU), ALIGN is?

A

The system levels and aligns the platform. Once complete, the READY NAV light goes on. The aircraft must be stationary during the alignment process.

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15
Q

in an INS alignment the accelerometers do?

A

Levelling

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16
Q

In INS alignment, what is caging?

A

Gimbals are driven to 900 to one another, voltage applied to heat oil, gyros brought up to speed.

17
Q

How long does alignment take on an INS?

A

17 Minutes

18
Q

How long does caging take on an INS alignment?

A

3 Minutes

19
Q

How long does levelling take on an INS alignment?

A

3 Minutes

20
Q

How long does gyrocompassing take on INS alignment?

A

11 minutes

21
Q

An INS does not calculate?

A

Longitude

22
Q

With longitude:

Two repeated crew inputs different from the stored value?

A

The system accepts the new value.

23
Q

With latitude:

Two repeated crew inputs different from the calculated value?

A

The system does not complete alignment.

24
Q

An INS does not compute its?

A

Longitude - you have to input it

25
Q

An INS consists of?

A
  • A platform
  • a standalone computer (navigation information)
26
Q

In ATT mode what information do you get?

A

Attitude reference still available, attitude reference for AI and Autopilot - System cannot be aligned in flight (navigation ability lost)

27
Q

Two types of errors with an INS?

A

Bounded and unbounded errors

28
Q

What is the typical error for an INS?

A

1 - 2 Nm/hr (can wonder off)

29
Q

The INS positional error of 1 – 2 NM/hr is dependent on factors affecting the accuracy of the platform, such as:

A
  • The gyro drift rate
  • Accelerometer bias
  • Misalignment of the platform
  • Computational errors
30
Q

The Inertial Navigation System + Air Data Computer = ?

A

Air Data Inertial Reference Unit (ADIRU)

31
Q

The INS needs the ____ from the ADC in order to calculate the wind information.

A

TAS

32
Q

After first integration, the speeds are
measured along E/W (known as U)
and N/S (known as V).

Adding the speeds as vectors gives
us a resultant ground speed…

…and a track as the resultant speed
will have an angle clockwise from
north.

A
33
Q

Fly By associated with the __ mode?

A

Auto

34
Q

Fly over assciated with the ____ mode?

A

Manual

35
Q

What is the cross track position and tracking error?

A