Inertial Navigation Flashcards

1
Q

INS do (not) require external input to compute position

A

not

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2
Q

With ___ from the ADC, they can calculate wind velocity

A

TAS

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3
Q

INS can work ___ and are (not) undetectable

A

anyway, they are

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4
Q

They can apply local variation between __N and __S from a table in the database, meaning a flux detector is not required

A

73 65

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5
Q

If the variation table cannot update the output from true to magnetic, then the set might show either ___ ___ or switch to ___

A

HDG FAIL TRUE

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6
Q

The difference between WGS84 and the oblique spheroid of the Earth is why ___ ___ is required

A

Schuler Tuning

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7
Q

Outline the general principle of Inertial Navigation

A
  • Start from a known position

- Calculate present position from directions and speed since then.

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8
Q

The drift should be around _nm per hour for a strapdown system

A

1

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9
Q

The drift could be _nm per hour for a stable platform

A

3

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10
Q

The main cause of cumulative distance errors come from wander in the ___ ___ and ___ ___ in the second stage of integration

A

levelling gyros, integration errors

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11
Q

The accuracy of any computed altitude decreases ___ with time

A

exponentially

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12
Q

As the accuracy degrades over time, supplementation with ___/___ is required, where it becomes subject to bound errors based on the other system

A

GPS/navaids

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13
Q

As the system error keeps growing, it is ___, and readings will be inaccurate to some extent

A

unbounded

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14
Q

The position will be most inaccurate at the top of ___, and just after ___

A

descent take off

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15
Q

Map shift occurs when the ___

A

moving map changes position to show the updates

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16
Q

Manual updating of the system is only allowed within __nm of a colocated VOR/DME, or above a visual fix below ___ft

A

25 5000

17
Q

Auto updating can take place within __nm of 2 DMEs, or ___nm of a single DME

A

200 140

18
Q

GPS is ___ accurate, with low bandwidth

A

more

19
Q

Low bandwidth means it has a ___ update rate

A

slow

20
Q

IRS and INS are ___ bandwidth systems.

A

high

21
Q

There will be ___ INS/IRS systems on modern aircraft

A

3

22
Q

The three types of coupling between GPS and INS are:

A

Uncouple, loosely, tightly

23
Q

Inertial systems have there own __V DC batteries which run for __ to __ minutes, or they may use a hot bus.

A

28 20 30

24
Q

If power is lost, you ___ realign for the rest of the flight

A

cannot

25
Q

Older systems were called INSs because that was their main function, modern versions are fully integrated with other systems, so known as ___

A

IRSs

26
Q

The output data of an IRS is:

A
  • True Track
  • Position
  • True heading
  • Attitude