Title:Fault tolerance analysis method for spacecraft attitude control system with intermittent faults

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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:ZL201210242175.4

Authorization number:ZL201210242175.4

Number of Inventors:4

Service Invention or Not:no

Application Date:2012-07-12

Authorization Date:2015-07-29