33th Congress of the International Council of the Aeronautical Sciences

07 - Systems, Subsystems and Equipment

AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT

H. Li, China; Z. Zhao, China; Z. Wan, China; L. Xu, China; S. Zhao, China; P. Sun, China

The concept of the starter/generator systemas a promising approach has been widely accepted in aircraft. An integrated control scheme is proposed to regulate the engine and output voltage of aircraft when starter/generator operates in different modes. Extensive simulation results are provided to confirm the validity and effectiveness of the proposed control scheme for in more electric aircraft.


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