11 Facts About Missile guidance

Missile guidance refers to a variety of methods of guiding a missile or a guided bomb to its intended target.

Concept of unmanned Missile guidance originated at least as early as World War I, with the idea of remotely guiding an airplane bomb onto a target, such as the systems developed for the first powered drones by Archibald Low .

CLOS Missile guidance is used mostly in shortrange air defense and antitank systems.

Proportional navigation is a guidance principle used in some form or another by most homing air target missiles.

Whatever the mechanism used in a go-onto-location-in-space Missile guidance system is, it must contain preset information about the target.

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Navigational Missile guidance is any type of Missile guidance executed by a system without a target tracker.

All of the guidance components are contained within the missile, and no outside information is used.

Inertial guidance uses sensitive measurement devices to calculate the location of the missile due to the acceleration put on it after leaving a known position.

Many civilian aircraft use inertial Missile guidance using a ring laser gyroscope, which is less accurate than the mechanical systems found in ICBMs, but which provide an inexpensive means of attaining a fairly accurate fix on location .

Inertial guidance is most favored for the initial guidance and reentry vehicles of strategic missiles, because it has no external signal and cannot be jammed.

Additionally, the relatively low precision of this Missile guidance method is less of an issue for large nuclear warheads.