Title:
GUIDED AIRFRAME
Document Type and Number:
Japanese Patent JPH06241696
Kind Code:
A
Abstract:
PURPOSE: To improve the ability of a guided airframe to track and be guided by preventing an optical sensor from being saturated with sun light which strikes the optical sensor.
CONSTITUTION: A guided airframe is provided with a limiter circuit 12, a bias signal generating circuit 13 and an adder 14. When sun light strikes an optical sensor, the flying body changes its flying path. Thus, the ability of the airframe to track and be guided is improved.
Inventors:
KIMOTO KENJI
Application Number:
JP3027193A
Publication Date:
September 02, 1994
Filing Date:
February 19, 1993
Export Citation:
Assignee:
MITSUBISHI ELECTRIC CORP
International Classes:
F41G7/22; F42B10/64; F42B15/01; G01S3/786; G05D1/12; B64C13/18; (IPC1-7): F41G7/22; B64C13/18; F42B10/64; F42B15/01; G01S3/786; G05D1/12
Attorney, Agent or Firm:
Takada Mamoru
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