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Τι (ποιος) είναι inertial guidance - ορισμός
VARIETY OF METHODS OF GUIDING A MISSILE
Command line-of-sight; Radio command guidance; Missile guidance system; ACLOS; Seeker-head; Homing (missile guidance); Stellar-inertial guidance; Astro-inertial guidance; Inertial missile guidance; Passive homing; Command to line-of-sight; Stellar inertial guidance; Stellar inertial guidance system; Astroinertial; Weapon guidance; Optical guidance; Electro-optical guidance; Munition guidance; Missile seeker; Missile tracking; Astrocelestial; Seeker head; GOLIS systems; GOT systems; Target tracking; Remote controlled missile; Guided warhead; Command to line-of-sight guidance; Target and missile tracking
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Inertial navigation system
![S3]].](https://commons.wikimedia.org/wiki/Special:FilePath/Centrale-intertielle missile S3 Musee du Bourget P1010652.JPG?width=200 "S3]].")
![The quartz rate sensor inside an [https://web.archive.org/web/20100419014447/http://en.wikipedia.org/wiki/E-Sky_Lama_model_helicopters E-Sky] model helicopter](https://commons.wikimedia.org/wiki/Special:FilePath/Gyro chip-Esky-Lama v3 model helicopter.jpg?width=200 "The quartz rate sensor inside an [https://web.archive.org/web/20100419014447/http://en.wikipedia.org/wiki/E-Sky_Lama_model_helicopters E-Sky] model helicopter")
![Principle of open loop [[accelerometer]]. Acceleration in the upward direction causes the mass to deflect downward.](https://commons.wikimedia.org/wiki/Special:FilePath/Pendular accel.svg?width=200 "Principle of open loop [[accelerometer]]. Acceleration in the upward direction causes the mass to deflect downward.")
CONTINUOUSLY COMPUTED DEAD RECKONING
Inertial navigation; Inertial guidance; Strapdown; Inertial tracking device; Sdins; SDINS; Inertial reference system; Inertial Navigation System; Inertial navigation unit; Inertial Navigation; Inertial Reference System; Inertial guidance system; Fluid-suspended gyrostabilized platform; Gimballed gyrostabilized platform; Strapdown inertial navigation; Strapdown inertial guidance; History of inertial navigation; Inertial motion tracking; Inertial positioning system
An inertial navigation system (INS) 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.
Inertial confinement fusion
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BRANCH OF FUSION ENERGY RESEARCH
Inertial fusion energy; Laser fusion; Inertial confinement; Laser inertial confinement; Inertial Fusion Energy; 4 pi laser; Inertial fusion; D-D Inertial Fusion; User:Warlord10327!/D-D Inertial Fusion
Inertial confinement fusion (ICF) is a fusion energy research program that initiates nuclear fusion reactions by compressing and heating targets filled with thermonuclear fuel. In modern machines, the targets are small spherical pellets about the size of a pinhead typically containing a mixture of about 10 milligrams of deuterium 2H and tritium 3H.
Stand guidance system
Visual Docking Guidance System; Safedock; AGNIS; Parallax Aircraft Parking Aid; AVGDS; A-VGDS; Visual Guidance Docking System; Stand guidance systems; A-VDGS; AVDGS
A stand guidance system is a system which gives information to a pilot attempting to park an aircraft at an airport stand, usually via visual methods, leading to the term Visual Docking Guidance System (VDGS) and also A-VDGS (the A standing for advanced) This allows them to remain clear of obstructions and ensures that jetways can reach the aircraft.
Βικιπαίδεια
Missile guidance
Missile guidance refers to a variety of methods of guiding a missile or a guided bomb to its intended target. The missile's target accuracy is a critical factor for its effectiveness. Guidance systems improve missile accuracy by improving its Probability of Guidance (Pg).
These guidance technologies can generally be divided up into a number of categories, with the broadest categories being "active", "passive", and "preset" guidance. Missiles and guided bombs generally use similar types of guidance system, the difference between the two being that missiles are powered by an onboard engine, whereas guided bombs rely on the speed and height of the launch aircraft for propulsion.
Παραδείγματα από το σώμα κειμένου για inertial guidance
1. Agni III has an inertial guidance system with improved optical or radar terminal phase correlation capability to guide it accurately to its target.
2. The missile could be deployed using rail or road mobile launch vehicles and had an inertial guidance system with improved optical or radar terminal phase correlation capability to guide it accurately to its target.
3. The 1'74 document describes the Jericho project, from its inception in France through its migration to Israel to the replacement of the original inertial guidance system by an Israeli design "based on components produced in Israel under licenses from U.S. companies." Israel Aircraft Industries is responsible for the development of the missile and has constructed a number of facilities for production and testing north of Tel Aviv, near Haifa, at Ramle and nearby it "a missile assembly and checkout plant." On Iran, the 1'74 NIE said, "there is no doubt of the Shah‘s ambition to make Iran a power to reckon with.