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Improvement of the Aircraft Design process for Air Traffic Management evaluations

机译:改进用于空中交通管理评估的飞机设计过程

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In the field of Aircraft Design, new transport concepts rely heavily on aero-propulsive effects with the objective of providing step changes in terms of energy consumption. Given the strong dependency of the level of lift with respect to engine settings, there is an added value for the designers to complete full simulations of the operational mission to verify the viability of the selected architecture. Regarding Air Traffic Management, the need for more accurate trajectories as well as solutions to characterize new aircraft in the air space has been identified. Taking the opportunity of these shared requirements, the authors present in this paper the coupling between a conceptual design sizing tool and an ATM simulator. The objective is to pave the way for future optimizations of the global system where aircraft would be designed taking into account real flight routes defined by ATM constraints. To validate the simulation model generated by the sizing code, resulting climb trajectories as well as initial cruise phases are compared with real flight traces recorded with an ADS-B antenna.
机译:在飞机设计领域,新的运输概念在很大程度上依赖于航空推进作用,目的是在能耗方面提供逐步的改变。考虑到升程水平与发动机设置之间的强烈依赖关系,设计者可以通过附加值来完成对运行任务的完整模拟,以验证所选架构的可行性。关于空中交通管理,已经确定了对更精确的航迹以及表征新飞机在空域中的解决方案的需求。利用这些共同需求的机会,本文的作者提出了概念设计尺寸调整工具和ATM仿真器之间的耦合。目的是为全球系统的未来优化铺平道路,在该系统中,飞机的设计应考虑到由ATM约束定义的实际飞行路线。为了验证由尺寸代码生成的仿真模型,将得到的爬升轨迹以及初始巡航阶段与用ADS-B天线记录的真实飞行轨迹进行比较。

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