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:
Feb. 21, 2017

Filed:

Jun. 30, 2014
Applicant:

Beijing Aerospace Wanda Hi-tech Ltd., Beijing, CN;

Inventors:

Qingbo Yu, Bejing, CN;

Jizhuo Men, Beijing, CN;

Shulun Zhao, Beijing, CN;

Rong Lang, Beijing, CN;

Xiaobin Liu, Beijing, CN;

Chunxiang Yang, Beijing, CN;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/36 (2006.01); G05D 1/00 (2006.01); G05D 3/00 (2006.01); G06F 7/00 (2006.01); G06F 17/00 (2006.01); G01C 21/18 (2006.01); H01Q 3/02 (2006.01); H01Q 1/24 (2006.01); B64G 1/10 (2006.01); B64G 1/24 (2006.01);
U.S. Cl.
CPC ...
G01C 21/18 (2013.01); B64G 1/1014 (2013.01); B64G 1/24 (2013.01); H01Q 1/247 (2013.01); H01Q 3/02 (2013.01);
Abstract

A method for controlling an antenna of a mobile communication application system based on double quaternions in MEMS inertial navigation. The method comprises: introducing an antenna control quaternion based on a navigation attitude quaternion; in each interrupt cycle of a navigation computer, updating the two quaternions respectively using a carrier system measured by a gyroscope relative to a rotation vector of an ideal platform coordinate system; in each filter cycle, correcting the error of the navigation attitude quaternion respectively using a Kalman filter; according to the relationship between the attitudes determined by the two attitude quaternions, determining the angular speed in an antenna control instruction; and finally, driving a servo system to rotate at an antenna servo control angle converted by an antenna control quaternion attitude.


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