Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1989-11-15
1991-09-17
Hellner, Mark
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
364900, G06F 100
Patent
active
050487710
ABSTRACT:
A method and apparatus are disclosed for a reprogrammable program missile memory module 26 which is placed within a missile 14 in substantially the same manner as the currently used programmable read only memory. The reprogrammable program memory module 26 provides for remote writing of tactical program data thereto while allowing the missile 14 to remain in a substantially operational state.
REFERENCES:
patent: 4037202 (1977-07-01), Terzian
patent: 4660170 (1987-04-01), Hui et al.
patent: 4935881 (1990-06-01), Lowenson et al.
Brown C. D.
Denson-Low W. K.
Heald R. M.
Hellner Mark
Hughes Aircraft Company
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