Missile system incorporating a targeting aid for man-in-the-loop

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

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Details

244 312, 244 313, 244 314, F42B 1500

Patent

active

056053070

ABSTRACT:
A missile is remotely controlled by a person operating with a base controller that displays an image of an aim-point target. Simultaneously, the base controller displays, as an overlay, a prosecutable target locus that represents the outer boundary of the region that may be hit by the missile, in the event that a maximum change in the guidance commands were to be introduced at that moment. The prosecutable target locus depends upon missile performance capability and the location of the missile relative to the aim-point target, which are provided to the base controller.

REFERENCES:
patent: 3567163 (1971-03-01), Kepp et al.
patent: 4267562 (1981-05-01), Raimondi
patent: 4274609 (1981-06-01), Ferrier et al.
patent: 4611771 (1986-09-01), Gibbons et al.
patent: 4907763 (1990-03-01), Pinson
patent: 5042743 (1991-08-01), Carney
patent: 5379676 (1995-01-01), Profeta et al.

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