Title:A flexible underactuated spacecraft control system and its attitude control method based on switching 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:ZL201410714308.2

Authorization number:CN104460679

Number of Inventors:3

Service Invention or Not:no

Application Date:2014-11-28

Authorization Date:2018-05-08

First Author:Yang Hao

Disigner of the Invention:Zhao Dong,Jiang Bin