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inertial navigation system

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Also known as INS, intertial guidance system, inertial reference platform, inertial instrument, inertial measurement unit, Inertial Navigation System, INS, inertial guidance

continuously computed dead reckoning

In the Vinony graph

Within Vinony's link graph, inertial navigation system is referenced by 1,129 other articles, and connects out to global navigation satellite system, fiber-optic gyroscope and turn and slip indicator.

It is catalogued under topics including Aerospace engineering, Aircraft instruments and Avionics.

Its subject is documented across 37 Wikipedia language editions.

~36 min read

Encyclopedic overview

A 1950s inertial navigation control developed at MIT Comparison of accuracy of various navigation systems: the radius of the circle indicates the accuracy. A smaller radius corresponds to a higher accuracy

An inertial navigation system (INS; also inertial guidance system, inertial instrument) is a navigation device that uses motion sensors (accelerometers), rotation sensors (gyroscopes) and a computer to continuously calculate by dead reckoning the position, the orientation, and the velocity (direction and speed of movement) of a moving object without the need for external references. Often the inertial sensors are supplemented by a barometric altimeter and sometimes by magnetic sensors (magnetometers) and/or speed measuring devices. INSs are used on mobile robots and on vehicles such as ships, aircraft, submarines, guided missiles, and spacecraft. Older INS systems generally used an inertial platform as their mounting point to the vehicle and the terms are sometimes considered synonymous.

Excerpted from Wikipedia’s “inertial navigation system” article, available under the CC BY-SA 4.0 licence.

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