将商用飞机系统思想应用于产品运行支持系统研制过程中,从利益攸关方需要定义、功能分析、需求定义和适航约束限制、系统架构定义、接口定义、设计综合、验证确认到运行评审,完整地分析了产品运行支持系统研制的全过程,并给出产品运行支持系统全生命周期过程的模型与定义。该方法可以有效地将大型客机产品运行顶层需求分解至产品研制和运行支持系统研制需求中,并且通过过程集成以及技术集成将运行支持系统研制与飞机研制相结合,从而保证大型客机在满足适航型号合格审定(TC)和航空器评审(AEG)要求的同时,能够满足客户实际运行安全性和经济性需求。
Applying up-to-date system engineering approach to the development of commercial aircraft operation support system, this paper analyzes the complete process of operation support system development from stakeholder needs definition, function analysis, requirement definition and airworthiness constraints, system architecture definition, interface definition, design integration, verification & validation, and airworthiness operation review. A commercial aircraft operation support lifecycle process model is defined and illustrated. This approach effectively divides the top level aircraft operation requirements into the aircraft requirements and operation support system requirements. By combining the aircraft development process with the operation support system development process through process integration and technical integration, this approach ensures the commercial aircraft meets not only the requirements of Type Certificate (TC) and Aircraft Evaluation Group (AEG), but also the airlines' requirements of safety and economical operation.
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