Title:
CONTROLLER FOR MISSILE
Document Type and Number:
Japanese Patent JP2719674
Kind Code:
B2
Abstract:
PURPOSE: To enhance a hitting accuracy by coping with demands for reductions in the size, weight and cost, and controlling (roughly) damping (convergence degree) of a body in lateral directions while correcting a time delay, an error, etc., caused at the time of rolling a body toward the target.
CONSTITUTION: A controller for a missile 2 has two main wings at outer periphery of an intermediate part, two steering wings 3 of a linear servomechanism on an outer periphery of a tail, and two steering wings 4 of a spoiler type steering mechanism in a directional position perpendicular to the wings 3.
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Inventors:
Kunitake Yasunari
Eiichiro Muto
Yoshihiko Nishida
Eiichiro Muto
Yoshihiko Nishida
Application Number:
JP30177192A
Publication Date:
February 25, 1998
Filing Date:
October 14, 1992
Export Citation:
Assignee:
Director General, Technical Research Division, Defense Agency
Kawasaki Heavy Industries, Ltd.
Kawasaki Heavy Industries, Ltd.
International Classes:
B64C9/02; B64C13/18; F42B10/64; F42B15/01; (IPC1-7): F42B10/64; B64C9/02; B64C13/18; F42B15/01
Domestic Patent References:
| JP4273999A | ||||
| JP3217798A | ||||
| JP618800U |
Attorney, Agent or Firm:
Yujiro Taka
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