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Patent Searching and Data


Title:
COMPASS SYSTEM
Document Type and Number:
Japanese Patent JPH02243917
Kind Code:
A
Abstract:

PURPOSE: To accurately measure the rotation of the magnetic field of the earth by providing a two-axial rate gyroscope for measuring the angular velocity of a vehicle, a suspension type magnetometer medium for measuring the magnetic field of the earth inside three orthogonal axes, a horizontal display unit, and a controller.

CONSTITUTION: The compass system 10 consists of the two-axial rate gyroscope 12 for measuring the angular velocity of the vehicle, the suspension type magnetometer medium 14 for measuring the magnetic field of the earth in the three orthogonal axes, the horizontal display unit 18, the controller 20 equipped with a mathematical central arithmetic unit which processes the output of an instrument and the input of operation to be performed and controls system operation, and a coupling device 22 for the operation to be performed which is equipped with a display for showing flight direction data on the vehicle and other system data and a medium for making a person who operates input instructions. Then the device 22 makes the person who operates input instructions for starting, controlling, and ending the system. Further, the person is made to receive data, based upon the instrument, which are generated by the system including a flight direction. Furthermore, the person is made to receive data based upon the state of available operation of the system.


Inventors:
ANTONII UOORUPOODO
Application Number:
JP27190789A
Publication Date:
September 28, 1990
Filing Date:
October 20, 1989
Export Citation:
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Assignee:
BRITISH AEROSPACE
International Classes:
G01C19/42; G01C17/38; G01C19/00; G01C21/00; (IPC1-7): G01C19/42
Attorney, Agent or Firm:
Shigeru Yagita (3 outside)



 
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