A modelling and simulation framework for the integrated design of aircraft systems

被引：1

作者：

Cimmino, N. ^{[1
]}

Ponnusamy, S. S. ^{[2
]}

Garriga, A. Garcia ^{[2
]}

Mainini, L. ^{[2
]}

机构：

[1] Univ Napoli Federico II, Dept Ind Engn, Naples, Italy

[2] United Technol Res Ctr UTRC, Cork, Ireland

来源：

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | 2020年 / 234卷 / 10期

基金：

欧盟地平线“2020”;

关键词：

Aircraft systems; aircraft-system integration; integrated design; landing gear; modelling and simulation; model based system engineering; multidisciplinary design optimization; OPTIMIZATION;

D O I：

10.1177/0954410019835726

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

New technologies and complex systems are being developed in commercial aviation to meet strict requirements regarding fuel consumption, emissions and noise constraints. This motivates the development of multidisciplinary environments to efficiently manage the increasing complexity of the design process. Under the Clean Sky 2 initiative, the ModellIng and Simulation tools for Systems IntegratiON on Aircraft (MISSION) project aims to develop an integrated framework to holistically support the aircraft design, development and validation processes. Within the MISSION framework, this paper proposes a methodology to handle the integration between the aircraft level and the system level in the early phase of aircraft design. The methodology is demonstrated for the case of the Landing Gear System in the rejected take-off scenario.

引用

页码：1648 / 1660

页数：13

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