Performance Reliability Response Surface Method for Flight Control System of UAV

摘要：

Performance reliability response surface plays an important role in reliability quantitative design for flight control system of UAV (Unmanned Aerial Vehicle).Integrating reliability and performance design is implemented by building system integrating simulation model,which includes performance simulation model,disturbance model and universal interface. Based on mission demands and performance requirements, performance reliability response surface method (PRRSM) is proposed to support optimization of Design-Dependent Parameters (DDPs) in order to improve performance reliability for flight control system of UAV.Detailed steps of applying the proposed method are given.PRRSM is demonstrated through a flight control system of UAV.

关键词： PRRSM DDPs flight control system UAV

作者: Huadong Tian Shengkui Zeng Yunxia Chen Yi Pang

作者单位: Dept.of System Engineering of Engineering Technology Beijing University of Aeronautics and Astronautics Beijing 100191,China

会议类型: 国际会议

会议名称: 2009 8th International Conference on Reliability,Maintainability and Safety(第八届中国国际可靠性、维修性、安全性会议)

会议地点: 成都

会议语种:英文

页码: 236-240

在线出版日期: 2009-08-24（万方平台首次上网日期，不代表论文的发表时间）