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

17
Q

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

18
Q

GPS is ___ accurate, with low bandwidth

19
Q

Low bandwidth means it has a ___ update rate

20
Q

IRS and INS are ___ bandwidth systems.

21
Q

There will be ___ INS/IRS systems on modern aircraft

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.

24
Q

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

25
Older systems were called INSs because that was their main function, modern versions are fully integrated with other systems, so known as ___
IRSs
26
The output data of an IRS is:
- True Track - Position - True heading - Attitude