Title:Spacecraft closed-loop attitude control system based on redundant controller and its control method

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Affilication of Author(s):College of Automation Engineering

Scope of patent:China

School Sign:Nanjing University of Aeronautics and Astronautics

Type of Patent:Invent

State of Patent:Authorized patents

Application Number:ZL201310085377.7

Authorization number:ZL201310085377.7

Number of Inventors:4

Service Invention or Not:no

Application Date:2013-03-08

Authorization Date:2015-07-29

First Author:Yang Hao

Disigner of the Invention:Jiang Bin,Cheng Yuehua,Zhou Donghua