The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Apr. 03, 1990

Filed:

Oct. 06, 1987
Applicant:
Inventors:

Uwe Krogmann, Uberlingen, DE;

Jurgen Bessel, Uberlingen, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G01C / ; G05D / ;
U.S. Cl.
CPC ...
364434 ; 364453 ; 364559 ; 364566 ; 33321 ; 244177 ; 244194 ; 73504 ;
Abstract

A plurality of two-axis rate gyros are arranged in relation to an aircraft-fixed coordinate system such that they redundantly supply angular rate information. A plurality of accelerometers supply correspondingly redundant acceleration information. First signal processing means comprise means for failure detection and elimination, such that angular rate and acceleration information subjected to error are eliminated. The angular rate and acceleration information thus cleared from errors supply stabilization signals for the autopilot. Second signal processing means obtain the angular rate and acceleration information cleared from errors and integrated if required, and therefrom supply heading and attitude reference signals.


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Krogmann, Uwe. (1990). Integrated redundant reference system for the flight control and for (U.S. Patent No. 4914598). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/4914598

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