Inertial Navigation Systems Flashcards

1
Q

How many accelerometers are in an INS?

A

2, one facing N-S, one facing E-W

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2
Q

What 3 laws does an INS work off?

A

Newtons 3 laws, if you know 2 factors, you know the other (Speed Distance Time triangle)

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3
Q

Why is the initial position in the INS required to be accurate?

A

Because the system applies acceleration, bearing, and velocity changes from this position. Therefore if this position is wrong, the system will be wrong until updated in the air.

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4
Q

Does gravity have an effect on the INS?

A

If it wasn’t for the gyroscopes installed, then yes! But overall no

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5
Q

What is earth rate compensation?

A

Because we want the accelerometers to be horizontal to the earth, they need to be tipped at a rate proportional to the earth’s rotation.

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6
Q

Is latitude or longitude being compensated for with earth rate?

A

Latitude. Maximum at the equator.

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7
Q

What is transport rate?

A

Compensation longitudinally in order to keep the accelerometer horizontal to the earth. It is based off velocity.

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8
Q

Is the INS aligned to true north or magnetic north?

A

True north

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9
Q

What is the disadvantage of a north-pointing INS system?

A

Can’t be used in polar regions, need to have a wander azimuth inertial system

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10
Q

In a wander azimuth inertial system, how are the accelerometers angled?

A

EW and NS, but with a wander angle.

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11
Q

Up to what radial error rate can an INS/IRS experience before being considered unserviceable

A

3+3t nm (t=number of hours of operation)

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12
Q

What is the maximum time you can navigate with a single IRS/INS?

A

10hrs since last alignment, must have backup. 3hrs nav in CTA, and 5hrs in oceanic areas

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13
Q

What is the maximum time you can navigate with two or more IRS/INS?

A

5hrs CTA, 12hrs OCTA or oceanic. Must be aligned within 10hrs

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14
Q

When can an IRS/INS be manually updated?

A

Overhead a VOR, within 25nm of a VOR/DME, or a visual fix <5000ftAGL

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15
Q

When can an IRS/INS be automatically updated?

A

within 140nm of a DME, or 200nm or two DMEs (DME/DME fix), <25nm from a VOR/DME

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16
Q

How many laser gyros are required for each IRS?

A

3 (pitch, roll yaw). therefore an aircraft with 3xIRS, would have 9 laser gyros.

17
Q

What are the advantages of an IRS (laser ring) compared to an INS (gyros)

A

No moving parts, more time between failure, less power, and provides info to more systems.