Title :
Performance reliability response surface method for flight control system of UAV
Author :
Tian, Huadong ; Zeng, Shengkui ; Chen, Yunxia ; Pang, Yi
Author_Institution :
Dept. of Syst. Eng., Beihang Univ., Beijing, China
Abstract :
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.
Keywords :
aerospace control; optimisation; reliability theory; remotely operated vehicles; design-dependent parameters; disturbance model; flight control system; optimization; performance simulation model; reliability quantitative design; reliability response surface method; system integrating simulation model; universal interface; unmanned aerial vehicle; Aerospace control; Aerospace simulation; Analytical models; Buildings; Constraint optimization; Control systems; Design optimization; Performance analysis; Response surface methodology; Unmanned aerial vehicles; DDPs; PRRSM; UAV; flight control system;
Conference_Titel :
Reliability, Maintainability and Safety, 2009. ICRMS 2009. 8th International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-4903-3
Electronic_ISBN :
978-1-4244-4905-7
DOI :
10.1109/ICRMS.2009.5270200
