Title:
ATTITUDE CONTROLLER FOR AEROPLANE
Document Type and Number:
Japanese Patent JPS62285017
Kind Code:
A
Abstract:
1. Arrangement in aircraft for generating triple redundant information for an assessment by majority decision for at least two horizontal axes in space with two strap-down gyroscope devices which are arranged to be rigidly fixed in space relative to one another, with two two-axis gyroscopes (1, 2) arranged perpendicular to one another with in each instance two measurement axes (M11 , M12 , and M21 , M22 respectively), of which a total of six measurement axes are arranged in the horizontal plane, and with systems for stabilising and regulating the flight attitude, characterised in that the six measurement axes are arranged differently, in order to be able to obtain redundant information for each of the two horizontal axes in space by computational allocation of in each instance three of the horizontal measurement axes to the respective horizontal axis.
Inventors:
BUORUFUGANGU HATSUSENPUFURUGU
Application Number:
JP12564687A
Publication Date:
December 10, 1987
Filing Date:
May 22, 1987
Export Citation:
Assignee:
LITEF LITTON TECH HELLIGE
International Classes:
B64D43/00; G01C21/16; G05D1/00; G05D1/08; (IPC1-7): B64D43/00; G01C21/16
Attorney, Agent or Firm:
Fujiya Shiga