Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1990-03-01
1991-08-06
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F42B 1066
Patent
active
050370405
ABSTRACT:
A fin stabilized subammunition body including a target detection device and being ejectable in a target area from a spin stabilized artillery carrier projectile. The target detection device includes a fixed sensor for detecting a target and producing target signals representing characteristics of the detected target, a reference platform for producing inertial reference signals, and a controller connected to the fixed sensor and the reference platform for producing drive control signals for selectively actuating a plurality of microreaction drive mechanisms arranged for producing transverse acceleration forces for aligning the body with a detected target.
REFERENCES:
patent: 3282540 (1966-11-01), Lipinski
patent: 3304434 (1962-05-01), Swaim et al.
patent: 4533094 (1985-08-01), Geis et al.
patent: 4568040 (1986-02-01), Metz
patent: 4598884 (1986-07-01), Speer
Goltz Gerhard
Grosswendt Werner
Peller Helmut
Seidensticker Jens
Jordan Charles T.
Rheinmetall GmbH
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