GA-based decentralized controller design for integrated flight/propulsion systems

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.

参考文章(8)
Jiyang Dai, Jianqin Mao, ROBUST FLIGHT CONTROLLER DESIGN FOR HELICOPTERS BASED ON GENETIC ALGORITHMS IFAC Proceedings Volumes. ,vol. 35, pp. 73- 78 ,(2002) , 10.3182/20020721-6-ES-1901.00347
M Yasar, A Ray, J F Horn, A comprehensive control strategy for integrated flight/propulsion systems: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. ,vol. 222, pp. 843- 859 ,(2008) , 10.1243/09544100JAERO297
S. Garg, Partitioning of centralized integrated flight/propulsion control design for decentralized implementation IEEE Transactions on Control Systems and Technology. ,vol. 1, pp. 93- 100 ,(1993) , 10.1109/87.238402
Zhenyang Chen, Petros G. Voulgaris, Decentralized Design for Integrated Flight/Propulsion Control of Aircraft Journal of Guidance, Control, and Dynamics. ,vol. 23, pp. 1037- 1044 ,(2000) , 10.2514/2.4672
Sarah Gatley, Declan Bates, Ian Postlethwaite, Partitioning and re-design of H-infinity loop shaping integrated flight and propulsion control systems AIAA Guidance, Navigation, and Control Conference and Exhibit. ,(2001) , 10.2514/6.2001-4384
Dai Ji, ROBUST FLIGHT CONTROLLER DESIGN FOR HELICOPTERS BASED ON GENETIC ALGORITHMS Acta Aeronautica Et Astronautica Sinica. ,(2001)