首页> 外文会议>European rotorcraft forum >CHALLENGE OF MODERN HELICOPTER COCKPIT
【24h】

CHALLENGE OF MODERN HELICOPTER COCKPIT

机译:现代直升机驾驶舱的挑战

获取原文

摘要

The extraordinary development of electronic and computing resources in the last decade has led to a significant increase in number and complexity of the avionics systems embedded on modern helicopters. The corresponding design & development process is thus facing the following challenge: to provide the crew with an easy access to an always increasing volume of information and functions, while maintaining the workload at the lowest possible level. Moreover, this development process has to cope with more and more severe schedule and budgetary constraints. In order to meet this challenge, Eurocopter has adopted since several years a new approach with prototyping and simulation techniques based on efficient computer aided design & specification tools. These tools use high level formal language and technical data base management. Their sound implementation allows upstream prototyping and simulation while providing full permanent technical control of the data flows within and between the different system constituents. This methodology supports a "crew centered design" approach with early pilot-in-the-loop validation, thus ensuring optimum fulfillment of the user's needs. An essential aspect of the specification through formal language is the associated Automatic Code Generation (ACG) capability. Its use allows a significant reduction of the software development cycle, not only for engineering simulation and testing, but also for embedded code generation when using qualified generators. A key point of the combined use of ACG and simulation is the "single digital specification principle". The whole method contributes to reduce the number of engineering iterations as well as their duration, while avoiding any discrepancy between simulation and embedded code. It brings therefore significant gains from technical, schedule and cost standpoints. It also leads to a reduction of Life Cycle Costs by making further software evolutions easier and contributes to an optimum synergy between engineering and training simulations. The paper will present how this development methodology is being applied on development programs such as NH90 and EC225/725, highlighting the current benefits and the expected trends for the future.
机译:过去十年的电子和计算资源的非凡发展导致嵌入现代直升机上的航空电子系统的数量和复杂性大幅增加。因此,相应的设计和开发过程因此面临以下挑战:提供船员,轻松访问始终增加的信息和功能,同时将工作量保持在可能的最低水平。此外,这种发展过程必须应对越来越严峻的计划和预算限制。为了满足这一挑战,欧洲直升机自几年采用了一种新方法,采用了基于高效计算机辅助设计和规范工具的原型设计和仿真技术。这些工具使用高级正式语言和技术数据库管理。它们的声音实现允许上游原型设计和仿真,同时提供对不同系统成分内部和之间的数据流动的全永久技术控制。该方法支持具有早期导航循环验证的“船员中心设计”方法,从而确保了对用户需求的最佳实现。通过正式语言的规范的重要方面是相关的自动代码生成(ACG)能力。它的使用允许大幅减少软件开发周期,不仅用于工程仿真和测试,还可以在使用合格发生器时进行嵌入式代码生成。联合使用ACG和仿真的关键点是“单一数字规范原理”。整个方法有助于减少工程迭代的数量以及它们的持续时间,同时避免模拟和嵌入式代码之间的任何差异。因此,它从技术,时间表和成本观点带来了显着的收益。它还通过进一步的软件演变更容易地降低生命周期成本,并有助于工程和培训模拟之间的最佳协同作用。本文将介绍该开发方法如何应用于NH90和EC225 / 725等开发计划,突出了当前的福利和未来的预期趋势。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号