| 摘要 |
PROBLEM TO BE SOLVED: To provide a control device solving nonconformity of a conventional control device, wherein the direction and the attitude are controlled by an aerodynamic steering vane and a thrust deflection body to be disposed after completing the control, such as being unusable for the flying body whose aerodynamic steering vane and thrust deflection body are separated from each other, in the direction and attitude control device for a flying object interlocking and simultaneously controlling the direction and the attitude of the flying object. SOLUTION: This direction and attitude control device for the flying body is provided with a support fixture which is provided in the outer circumferential surface of a machine body for installing the thrust deflection part and pivotally supports the rear end part of a joint swinging following to the aerodynamic vane, a support mount installed in the outer circumference of the thrust deflection vane and pivotally supporting an arm fixed to a rotary shaft of the thrust deflection vane, and a long transmission element disposed between the joint and the arm, transmitting the swinging of the aerodynamic steering vane to the thrust force deflection vane, and composed of a soft material. Thereby, this control device can be used for the flying body whose thrust deflection part and aerodynamic steering part are disposed in a largely separated state in the machine body axial direction and control the direction and the attitude in simultaneously controlling the aerodynamic steering vane with the thrust deflection body without impairing the control by the aerodynamic steering part in a regular flying. COPYRIGHT: (C)2003,JPO
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