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:
Oct. 26, 2021

Filed:

Sep. 02, 2016
Applicant:

Aerospace Dongfanghong Development Ltd, Guangdong, CN;

Inventors:

Yimin Kou, Guangdong, CN;

Bibo Guo, Guangdong, CN;

Lijun Xue, Guangdong, CN;

Shilong Wei, Guangdong, CN;

Yanbo Ji, Guangdong, CN;

Qin Yuan, Guangdong, CN;

Yingchun Zhang, Guangdong, CN;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/24 (2006.01); G05B 17/02 (2006.01); G06F 17/13 (2006.01);
U.S. Cl.
CPC ...
B64G 1/242 (2013.01); G05B 17/02 (2013.01); B64G 2001/245 (2013.01); G06F 17/13 (2013.01);
Abstract

Provided is a single-axis pointing pure magnetic control algorithm for a spacecraft based on geometrical analysis to realize single-axis pointing control of the spacecraft through the pure magnetic control algorithm in which a magnetic torque is only output by a magnetorquer to interact with a geomagnetic field to generate a control torque. The algorithm uses a spatial geometry method to obtain an optimally controlled magnetic torque direction, thereby designing a PD controller. The problem that the traditional magnetic control method is low in efficiency and even cannot be controlled is overcome. The algorithm is simple and easy, can be used in the attitude control field of spacecrafts, and achieves the pointing control in point-to-sun of a solar array and point-to-ground of antennae.


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