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Since so many types of missile use this guidance system, they are usually subdivided into four groups: A particular type of command guidance and navigation where the missile is always to commanded lie on the line of sight (LOS) between the tracking unit and the aircraft is known as command to line of sight (CLOS) or three-point guidance.
Manual command to line of sight (MCLOS or MACLOS) [1] is a method for guiding guided missiles. With an MCLOS missile, the operator must track the missile and the target simultaneously and guide the missile to the target. Typically the missile is steered with a joystick, and its path is observed through a periscope-type telescopic sight.
The Chief of Engineers is the senior service engineer for the Department of Defense, responsible for integrating all aspects of combat, general and geospatial engineering across the Joint Force. The Chief of Engineers also commands the United States Army Corps of Engineers. As commander of the US Army Corps of Engineers, the Chief of Engineers ...
The main disadvantage of both SACLOS guidance systems in an anti-tank role is that working on angular differences evaluation, it does not allow any notable separation between guidance system and missile launch post the opposite of manual command to line of sight (MCLOS) ones, thus allowing updated version of such anti-tank weapons (notably AT-3 ...
Guidance, navigation and control (abbreviated GNC, GN&C, or G&C) is a branch of engineering dealing with the design of systems to control the movement of vehicles, especially, automobiles, ships, aircraft, and spacecraft. In many cases these functions can be performed by trained humans.
The guidance systems, the KMU-353 and KMU-390, were essentially re-packaged Maverick A-model seekers, while the KMU-359/B used the later IR imager version from the D-model Mavericks. When completely assembled, the seeker, guidance system and bomb were known as the GBU-8 , or GBU-9 when used with the 3,000 pounds (1,400 kg) Mark 118 bomb . [ 7 ]
[8]: 82 From flight of the 16th X-9 the rocket motor was a Bell XLR65-BA-1 [8]: 87 The X-9 Shrike was flown with two different guidance systems. The first was a radio command guidance system manufactured by RCA's Federal Telecommunications Division. Later in the development program guidance was provided by a preset/radar command guidance system ...
Television guidance (TGM) is a type of missile guidance system using a television camera in the missile or glide bomb that sends its signal back to the launch platform. There, a weapons officer or bomb aimer watches the image on a television screen and sends corrections to the missile, typically over a radio control link.