作者: Dai Jiyang , Huang Ying , Peng Chen
DOI: 10.1109/PEAM.2012.6612523
关键词:
摘要: A new method is developed to deal with the problem that a decentralized integrated flight/propulsion control system needs keep centralized performance. The systematic procedure emphasizes quickly finding subcontrollers matching closed-loop performance characteristics of controller, which featured by fact GA used optimize design H-infinity controller and engine subcontroller, only one interface variable satisfy requirement. optimization motivated implementation issues where it desirable reduce time in trial error process accurately find best subcontrollers. applied for short take-off landing fighter. Through comparing simulation results those system, match command tracking decoupling achieved control.