Title:
【発明の名称】飛しょう体の誘導制御装置
Document Type and Number:
Japanese Patent JP2712861
Kind Code:
B2
Abstract:
PURPOSE:To obtain a guidance control device capable of calculating a guidance signal in high accuracy regardless of the characteristics of each radome by correcting the bore sight error of radome corresponding to the angle of an antenna. CONSTITUTION:An angle detector 9 for detecting the angle to a missile is fixed on an antenna 7. Bore sight error is calculated with a correction calculator 10 by following the angle signal obtained from this angle detector. By using an error angle signal obtained from an error angle detector 2, a correction signal can be subtracted. Thus, by subtracting the correction signal from the error angle, a high accuracy guidance signal can be obtained regardless of the bore sight error characteristics of a radome.
Inventors:
Kazuhiro Ueda
Application Number:
JP6160491A
Publication Date:
February 16, 1998
Filing Date:
March 26, 1991
Export Citation:
Assignee:
Mitsubishi Electric Corporation
International Classes:
F42B10/46; F42B15/01; G01S3/10; G01S3/38; G05D1/12; F41G7/22; (IPC1-7): G01S3/10; F41G7/22; F42B10/46; F42B15/01; G01S3/38; G05D1/12
Domestic Patent References:
| JP370997A | ||||
| JP1305381A | ||||
| JP63282498A | ||||
| JP6100652B2 |
Other References:
【文献】特許2518465(JP,B2)
Attorney, Agent or Firm:
Kaneo Miyata (3 outside)