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Advanced aircraft performance modeling for ATM: Analysis of BADA model capabilities

机译:用于ATM的高级飞机性能建模:BADA模型功能分析

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This paper provides an analysis of the BADA aircraft performance model capabilities and addresses the BADA model ability to provide accurate modeling of aircraft performances over the complete flight envelope for a number of aircraft types and different ways in which an aircraft can be operated during the flight. The focus of the paper is the support of complex aircraft operations by BADA. A short description of the two existing BADA families and their main characteristics is given. The complex flight instructions and operating regimes — economy climb, cruise and descent based on cost index, maximum range cruise, long range cruise, optimum altitude and maximum endurance cruise — identified as key features in support to optimized flight execution are discussed. The optimization procedures and equations in which they derive are presented and the ability of the BADA model to support these flight operations is demonstrated. It is shown that BADA 4 can be successfully used with complex instructions and operating regimes, whereas the use of BADA 3 is limited. Finally, the results of a validation experiment dedicated to BADA thrust models are presented.
机译:本文提供了对BADA飞机性能模型功能的分析,并探讨了BADA模型的能力,该能力可以为多种飞机类型和在飞行过程中操作飞机的不同方式提供完整飞行范围内飞机性能的准确建模。本文的重点是BADA对复杂飞机运营的支持。简要介绍了两个现有的BADA系列及其主要特征。讨论了复杂的飞行指令和操作方式-基于成本指数的经济爬升,巡航和下降,最大距离巡航,远程巡航,最佳高度和最大耐力巡航-被确定为支持优化飞行执行的关键特征。给出了推导它们的优化程序和方程式,并证明了BADA模型支持这些飞行操作的能力。结果表明,BADA 4可以成功地用于复杂的指令和操作机制,而BADA 3的使用受到限制。最后,介绍了专用于BADA推力模型的验证实验的结果。

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