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

fYear

2009

fDate

20-24 July 2009

Firstpage

236

Lastpage

240

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;

fLanguage

English

Publisher

ieee

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

Type

conf

DOI

10.1109/ICRMS.2009.5270200

Filename

5270200