Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1990-04-30
1991-11-19
Hellner, Mark
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F42B 1328
Patent
active
050659570
ABSTRACT:
A device for controlling an aerodynamic body having a searching head, a sensor and setting members for exerting a transversal force on the aerodynamic body into a target due to the sensor signals. In order to make possible a simple design of this device which can also be used for small aerodynamic bodies, the sensor and the setting members are arranged at a common rotor which rotates, driven about the longitudinal axis of the aerodynamic body, and can be influenced by means of a braking system as to its angular position relative to the aerodynamic body, generating a transversal force on the aerodynamic body.
REFERENCES:
patent: 4512537 (1985-04-01), Sebestyen et al.
patent: 4681283 (1987-07-01), Kranz
patent: 4898342 (1990-02-01), Kranz et al.
patent: 4966078 (1990-10-01), Schleimann-Jensen
Hellner Mark
Messerschmitt-Bolkow-Blohm GmbH
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