Inertial navigation

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	To oppose or discuss a nomination, please go to CZ:Proposed for deletion and follow the instructions. For the monthly nomination lists, see Category:Articles for deletion. Inertial navigation is a technique of [[navigation that does not depend on external references such as [[compasses, [[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 [[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 Does not require external navigation infrastructure Is resistant to [[electronic warfare Inertial navigation is well-established technique; it is not to be confused with the concept of [[inertial propulsion developed within the [[Russian space research program. 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 [[geodesy|geodetic coordinate system. Naval applications [[Compass#Gyrocompasses|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 [[United States Navy became concerned that it had multiple systems (i.e., [[AN-|AN/[[WSN-5 aboard surface combatants, the [[AN-|AN/[[WSN-3 aboard submarines and the [[AN-|AN/[[WSN-1 aboard aircraft carriers) where one would do, and that much less expensive [[commercial-off-the-shelf components were available. The [[AN-|AN/[[WSN-7 Ring Laser Gyro Navigation System, will replace all three, which are 15-20 years old and for which it is increasingly difficult to obtain spare parts. References