Title:
GPS誘導式兵器
Document Type and Number:
Japanese Patent JP4046942
Kind Code:
B2
Abstract:
A tail fin assembly for a munition having a housing configured for attachment to the munition, at least one flight control surface, an actuator for effecting movement of the flight control surface(s), so as to facilitate guiding of the munition, and a guidance system for controlling the actuator mechanism. The guidance system has a global positioning system (GPS) receiver for effecting control of the actuator mechanism.
Inventors:
Abbott, Anthony S.
Application Number:
JP2000502375A
Publication Date:
February 13, 2008
Filing Date:
May 20, 1998
Export Citation:
Assignee:
Northrop Grumman Corporation
International Classes:
F42B15/01; B64C5/02; G01C21/00; B64C13/20; F41G7/00; F41G7/34; F42B10/64; G01S5/14; G01S19/07; G01S19/11; G01S19/12; G01S19/18; G01S19/31; G01S19/41; G01S19/48; G01S19/53; G05D1/12; G08G1/0969; G01S5/00
Domestic Patent References:
| JP3113681B2 | ||||
| JP2625360B2 | ||||
| JP7005241A | ||||
| JP9134217A | ||||
| JP5019854A | ||||
| JP4002913A | ||||
| JP8248114A | ||||
| JP2060897A |
Attorney, Agent or Firm:
Hironobu Onda
Makoto Onda
Makoto Onda