You are seeing Ask web results for inertial guidance system.
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Inertial navigation system - Wikipedia, the free encyclopedia
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Hutchinson encyclopedia article about inertial guidance system. inertial guidance system. Information about inertial guidance system in the Hutchinson encyclopedia. ... An inertial guidance system developed for the X-20 was later used on the X-15 rockets, as was an electric, rather than hydraulic, flight control system.
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Guidance system - Wikipedia, the free encyclopedia
A guidance system is a device or group of devices used to navigate a ship, aircraft, missile, rocket, satellite, or other craft. Typically, this refers to a system that navigates without direct or c...
en.wikipedia.org/wiki/Guidance_system |
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Gemini Inertial Guidance System space exploration ... The major change in the flight control system from Titan II missile to Gemini launch vehicle was substitution of the General Electric Mod IIIG radio guidance system (RGS) and Titan I three-axis reference system for the Titan II inertial guidance system.
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INERTIAL GUIDANCE SYSTEM SIMPLIFIED ... The Inertial Guidance System uses deviations to generate error signal commands which instruct the aircraft to move from a position where it is to a position where it isn't, arriving at a position where it wasn't, or now is.
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The Inertial Guidance System uses deviations to generate error signal commands which instruct the aircraft to move from a position where it is to a position where it isn't, arriving at a position where it wasn't, or now is.
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The inertial navigation system (INS) is a self-contained unit that is located within an aircraft or rocket. It is programmed with its starting point and destination. An INS measures only movement; it does not measure airspeed or wind velocity.
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Abstract : A Montecarlo simulation is conducted to ascertain performance of the ATIGS system is a proposed air-launched cruise missile configuration. The simulation is conducted within a local-level inertial frame consisting of down-range, ... Descriptors : *KALMAN FILTERING, *CRUISE MISSILES, *INERTIAL GUIDANCE,
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Accession Number : AD0429393 ... Descriptive Note : Quarterly program progress rept., 1 Oct-31 Dec 63. ... Corporate Author : GENERAL MOTORS CORP MILWAUKEE WIS AC SPARK PLUG DIV...
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2487793 Object controlling electric motor system ... 2606448 Master gyroscope system ... 2638288 Control system for craft operable in space...
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