Inertial navigation: Difference between revisions

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'''Inertial navigation''' is a technique of [[navigation]] that does not depend on external references such as [[compass]]es, [[celestial navigation|stars]], [[gravity]] or [[GPS]], but computes the present position by sensing the movement of the navigating platform from a precisely known starting point in space. The general approach is to use multiple [[gyroscope]]s as references for the axes of position, as well as for error correction, with [[strain gauge]]s or other [[accelerometer]]s to sense the motion.
'''Inertial navigation''' is a technique of [[navigation]] that does not depend on external references such as [[compass]]es, [[celestial navigation|stars]], [[gravity]] or [[GPS]], but computes the present position by sensing the movement of the navigating platform from a precisely known starting point in space. The general approach is to use multiple [[gyroscope]]s as references for the axes of position, as well as for error correction, using [[accelerometer]]s to sense the motion.
 
There are two major types of inertial navigation sensors, gimballed, where the sensors can move, and strapdown, where they are bonded to the moving vehicle.


The method is exceptionally important for [[precision-guided munition]]s, [[space vehicle]]s, and military ships, submarines and aircraft, because it
The method is exceptionally important for [[precision-guided munition]]s, [[space vehicle]]s, and military ships, submarines and aircraft, because it
:*Does not require external navigation infrastructure
:*Does not require external navigation infrastructure
:*Is resistant to [[electronic warfare]]
:*Is resistant to [[electronic warfare]]
==Modes of operation==
*Space stable
*Local level north slaved
*Local level wander or free azimuth
*Two accelerometer local level
*Strapdown
In practice, inertial information is combined with other sources, such as [[GPS]] satellite.
==Enabling technologies==
==Enabling technologies==
[{Gyroscope]]s, first used as non-magnetic compasses and as [[true vertical indicator]]s in aviation, are the fundamental enabling technology. Inertial navigation greatly benefited when gyroscope technology moved beyond mechanical to ring laser techniques, which do not require moving parts and can be much smaller.
Essential to inertial navigation are gyroscopes, accelerometers, and computers, as well as the mathematics of inertial position comutation.
===Gyroscopes in inertial navigation===
[[Gyroscope]]s, first used as non-magnetic compasses and as [[true vertical indicator]]s in aviation, are the fundamental enabling technology. Inertial navigation greatly benefited when gyroscope technology moved beyond mechanical to optical techniques, which do not require moving parts and can be much smaller.  
 
Gyroscope-generated information includes:
*rate
*rate integrating
*single degree of freedom
*two degree of freedom gyro
===Mathematics===
Inertial navigation is referenced to a [[geodesy|geodetic]] coordinate system.
 
==Naval applications==
==Naval applications==
[[Gyrocompasses]] were precursors of full inertial navigation.
[[Gyrocompasses]] were precursors of full inertial navigation.

Revision as of 13:09, 2 March 2010

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Inertial navigation is a technique of navigation that does not depend on external references such as compasses, stars, gravity or GPS, but computes the present position by sensing the movement of the navigating platform from a precisely known starting point in space. The general approach is to use multiple gyroscopes as references for the axes of position, as well as for error correction, using accelerometers to sense the motion.

There are two major types of inertial navigation sensors, gimballed, where the sensors can move, and strapdown, where they are bonded to the moving vehicle.

The method is exceptionally important for precision-guided munitions, space vehicles, and military ships, submarines and aircraft, because it

Modes of operation

  • Space stable
  • Local level north slaved
  • Local level wander or free azimuth
  • Two accelerometer local level
  • Strapdown

In practice, inertial information is combined with other sources, such as GPS satellite.

Enabling technologies

Essential to inertial navigation are gyroscopes, accelerometers, and computers, as well as the mathematics of inertial position comutation.

Gyroscopes in inertial navigation

Gyroscopes, first used as non-magnetic compasses and as true vertical indicators in aviation, are the fundamental enabling technology. Inertial navigation greatly benefited when gyroscope technology moved beyond mechanical to optical techniques, which do not require moving parts and can be much smaller.

Gyroscope-generated information includes:

  • rate
  • rate integrating
  • single degree of freedom
  • two degree of freedom gyro

Mathematics

Inertial navigation is referenced to a geodetic coordinate system.

Naval applications

Gyrocompasses were precursors of full inertial navigation.

A first major implementation was the Ship Inertial Navigation System aboard the first U.S. ballistic missile submarines, which needed absolutely precise position information for accurate missile launching, but whose operational security depended on not exposing themselves for star sights, radio navigation, etc. While the submarine systems have continued to improve, and intertial navigation became common on surface warships, the U.S. Navy became concerned that it was developing multiple systems where one would do, and that much less expensive commercial-off-the-shelf components were available. [1]

References

  1. Ring Laser Gyro Navigator Project Team, Acquiring a Common NDI Ship/Submarine Inertial Navigation System, Naval Sea Systems Command, U.S. Navy