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An Engineering Optimization Method with Application to STOL-Aircraft Approach and Landing Trajectories

机译:一种适用于sTOL飞机进近着陆轨迹的工程优化方法

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摘要

An optimization method has been developed that computes the optimal open loop inputs for a dynamical system by observing only its output. The method reduces to static optimization by expressing the inputs as series of functions with parameters to be optimized. Since the method is not concerned with the details of the dynamical system to be optimized, it works for both linear and nonlinear systems. The method and the application to optimizing longitudinal landing paths for a STOL aircraft with an augmented wing are discussed. Noise, fuel, time, and path deviation minimizations are considered with and without angle of attack, acceleration excursion, flight path, endpoint, and other constraints. (Author)

著录项

  • 作者

    Jacob, H. G.;

  • 作者单位
  • 年度 1972
  • 页码 1-43
  • 总页数 43
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

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