Patent ReferencesCanard control assembly for a projectile Apparatus for correcting the flight path of a missile Missile with adjustable flying controls Projectile steering apparatus and method Patent #: 4966078 InventorAssigneeApplicationNo. 516516 filed on 04/30/1990US Classes:244/3.21Attitude control mechanismsExaminersPrimary: Hellner, MarkAttorney, Agent or FirmInternational ClassF42B 013/28Foreign Application Priority Data1986-02-27 DEAbstractA 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. | |