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Performance Reliability Response Surface Method for Flight Control System of UAV

机译:无人机飞行控制系统性能可靠性响应面法

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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.
机译:性能可靠性响应面在无人机飞行控制系统的可靠性定量设计中起着重要作用。集成可靠性和性能设计是通过构建集成了仿真模型的系统来实现的,仿真模型包括性能仿真模型,扰动模型和通用接口。基于任务需求和性能要求,提出了性能可靠性响应面法(PRRSM)来支持设计相关参数(DDP)的优化,以提高无人机飞行控制系统的性能可靠性。 PRRSM通过无人机的飞行控制系统进行了演示。

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