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Development of an optimization theory based tool (AutoPOM) for the Bell 427 helicopter simulation model validation.

机译:开发用于贝尔427直升机仿真模型验证的基于优化理论的工具(AutoPOM)。

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摘要

This thesis presented here is a part of work for Bell 427 helicopter simulator research project. The purpose of the research was to obtain a global simulation model which was a composition of several distinct simulation models of the Bell 427 helicopter in various flight conditions. The main tasks of our university team were the corrections of the raw flight test data and the simulation model validation.; The corrections of the raw flight test data were to reorganize the flight test data in standardized formats so that all partners could easily use it. The validation was to evaluate and approve the global simulation model in accordance with Advisory Circular AC 120-63. Our team used the software POM developed by NRC to validate the simulation model. Usually, one flight case validation process took about 4-6 hours or more by use of POM. In this research project, the software AutoPOM based on POM was developed. By use of AutoPOM, one flight case validation process took about 20-30 minutes in the computer (AMD Athlon(TM) XP 1800+, 1.53GHz, 512MB). This was 12 times faster than POM.; This thesis presents the helicopter mathematical model, corrections of the raw flight test data and the simulation model validation. The contribution of this thesis was the development of the software AutoPOM.; Validation process for flight cases by use of POM can be described as a mathematical multi-objective optimization problem. This problem can be expressed by a utility function of Least Square cost functions with their weights. Because the decision vector is different from the optimization vector, the expressions for the first partial derivatives of the objective function with respect to the decision vector can not be found. Thus the optimization problem can not be solved by indirect method, but it can be by direct methods and genetic algorithms. Three algorithms (Hooke and Jeeves' method, Nelder and Mead's method, and Genetic algorithm) were selected and applied to the software POM to develop the software AutoPOM. The AutoPOM interface is created by use of Matlab Graphical User Interface (GUI) techniques, which is clear and easy to use. This is an important criterion for engineers in industry.; Experimental results show that the three algorithms can solve the optimization problem. The Hooke and Jeeves' method starts from one point, its failure exploration steps delay the convergence speed. The Nelder and Mead's method starts from (n + 1) points; it uses more information from (n + 1) points and each step is forward to the convergence zoom. The Genetic Algorithm (GA) convergence speed varies due to random choice of the crossover sites and the mutation sites, the offspring may be worse than their parents, the convergence speed can be either fast or slow.; Based on the convergence speeds of the three algorithms, we recommend the use of the Nelder and Mead's method.
机译:本文介绍的论文是Bell 427直升机模拟器研究项目的一部分工作。该研究的目的是获得一个全局仿真模型,该模型由Bell 427直升机在不同飞行条件下的几种不同仿真模型组成。我们大学团队的主要任务是更正原始飞行测试数据和仿真模型验证。原始飞行测试数据的更正旨在以标准化格式重新组织飞行测试数据,以便所有合作伙伴都可以轻松使用它。验证是根据咨询通告AC 120-63评估和批准全局仿真模型。我们的团队使用了NRC开发的软件POM来验证仿真模型。通常,使用POM进行一次飞行案例验证过程大约需要4-6个小时或更长时间。在该研究项目中,开发了基于POM的AutoPOM软件。通过使用AutoPOM,一个飞行案例验证过程在计算机(AMD Athlon™XP 1800 +,1.53GHz,512MB)中花费了大约20-30分钟。这比POM快12倍。本文介绍了直升机的数学模型,原始飞行测试数据的校正和仿真模型的验证。本文的贡献是开发了AutoPOM软件。使用POM进行的飞行案例验证过程可以描述为数学上的多目标优化问题。这个问题可以用最小二乘成本函数的效用函数及其权重来表示。由于决策向量与优化向量不同,因此无法找到目标函数相对于决策向量的一阶偏导数的表达式。因此,优化问题不能通过间接方法解决,而可以通过直接方法和遗传算法解决。选择了三种算法(Hooke和Jeeves方法,Nelder和Mead方法以及遗传算法)并将其应用于软件POM以开发AutoPOM软件。 AutoPOM界面是使用Matlab图形用户界面(GUI)技术创建的,该技术清晰易用。这是工业工程师的重要标准。实验结果表明,这三种算法都能解决优化问题。 Hooke and Jeeves的方法从一点开始,其失败探索步骤延迟了收敛速度。 Nelder and Mead的方法从(n + 1)个点开始;它使用(n + 1)个点中的更多信息,并且每个步骤都将进行收敛缩放。遗传算法(GA)的收敛速度因交叉位点和突变位点的随机选择而异,后代可能比其父代更差,收敛速度可以快也可以慢。基于这三种算法的收敛速度,我们建议使用Nelder和Mead方法。

著录项

  • 作者

    Chen, Wen Hu.;

  • 作者单位

    Ecole Polytechnique, Montreal (Canada).;

  • 授予单位 Ecole Polytechnique, Montreal (Canada).;
  • 学科 Engineering Aerospace.
  • 学位 M.Sc.A.
  • 年度 2007
  • 页码 126 p.
  • 总页数 126
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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