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  2. Proportional navigation - Wikipedia

    en.wikipedia.org/wiki/Proportional_navigation

    Proportional navigation (also known as PN or Pro-Nav) is a guidance law (analogous to proportional control) used in some form or another by most homing air target missiles. [1] It is based on the fact that two vehicles are on a collision course when their direct line-of-sight does not change direction as the range closes. PN dictates that the ...

  3. Missile guidance - Wikipedia

    en.wikipedia.org/wiki/Missile_guidance

    Proportional navigation (also known as "PN" or "Pro-Nav") is a guidance principle (analogous to proportional control) used in some form or another by most homing air target missiles. [5] It is based on the fact that two objects are on a collision course when the direction of their direct line-of-sight does not change. PN dictates that the ...

  4. Guidance, navigation, and control - Wikipedia

    en.wikipedia.org/wiki/Guidance,_navigation,_and...

    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.

  5. Pursuit guidance - Wikipedia

    en.wikipedia.org/wiki/Pursuit_guidance

    In pursuit guidance, the missile is steered so that the velocity vector of the missile always points at the target, i.e. it has always the direction of the line of sight. This was the natural outcome of many guidance systems, notably beam riding systems where the missile followed the radar signal that was illuminating the target.

  6. Category:Missile guidance - Wikipedia

    en.wikipedia.org/wiki/Category:Missile_guidance

    Missile guidance — methods for in-flight guidance of guided missiles, after they have been launched. ... Proportional navigation; Pursuit guidance; Q. Q-guidance; S.

  7. FIM-92 Stinger - Wikipedia

    en.wikipedia.org/wiki/FIM-92_Stinger

    Guidance to the target is initially through proportional navigation, then switches to another mode that directs the missile towards the target airframe instead of its exhaust plume. There are three main variants in use: the Stinger Basic, Stinger-Passive Optical Seeker Technique (POST), and Stinger-Reprogrammable Microprocessor (RMP).

  8. Spacecraft attitude determination and control - Wikipedia

    en.wikipedia.org/wiki/Spacecraft_attitude...

    A spacecraft's attitude must typically be stabilized and controlled for a variety of reasons. It is often needed so that the spacecraft high-gain antenna may be accurately pointed to Earth for communications, so that onboard experiments may accomplish precise pointing for accurate collection and subsequent interpretation of data, so that the heating and cooling effects of sunlight and shadow ...

  9. Q-guidance - Wikipedia

    en.wikipedia.org/wiki/Q-guidance

    At the time Q-guidance was developed, the main competitive method was called Delta-guidance. According to Mackenzie, [1] Titan, some versions of Atlas, Minuteman I and II used Delta-guidance, while Q-guidance was used for Thor IRBM and Polaris, and presumably Poseidon. It appears, from monitoring of test launches, that early Soviet ICBMs used a ...