Process for the autonomous positional control of guided missiles

Details Process for the autonomous positional control of guided missiles Process for the autonomous positional control of guided missiles

1993-10-08

1995-03-14

Pihulic, Daniel T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 700

Patent

active

053970799

ABSTRACT:
Process for the autonomous positional control of guided missiles, which are to be launched from a carrier plane, but without the cooperation thereof, wherein data on the instantaneous position of the guided missile, as well as flight and target data are fed into a computer of the guided missile already on the ground. The initial data fed into the computer are continually updated with changing values from the inertial navigation and additional navigational aids and are further calculated to achieve autonomous flight guidance and self-guiding of the missile. An uninterruptible power supply of the guided missile is maintained beginning from the moment of data reception.

REFERENCES:
patent: 4470562 (1984-09-01), Hall et al.
patent: 5260709 (1993-11-01), Nowakowski

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