首页> 美国政府科技报告 >THEORETICAL AND ANALOG STUDIES OF THE EFFECTS OF NONLINEAR STABILITY DERIVATIVES ON THE LONGITUDINAL MOTIONS OF AN AIRCRAFT IN RESPONSE TO STEP CONTROL DEFLECTIONS AND TO THE INFLUENCE OF PROPORTIONAL AUTOMATIC CONTROL
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THEORETICAL AND ANALOG STUDIES OF THE EFFECTS OF NONLINEAR STABILITY DERIVATIVES ON THE LONGITUDINAL MOTIONS OF AN AIRCRAFT IN RESPONSE TO STEP CONTROL DEFLECTIONS AND TO THE INFLUENCE OF PROPORTIONAL AUTOMATIC CONTROL

机译:非线性稳定性导数对飞机纵向运动响应阶跃控制偏差影响的理论模拟研究及比例自动控制的影响

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摘要

A study has been made of the effect of two nonlinear stability derivatives, caused by the nonlinear variations of pitching moment and lift coethcient s with angle of attack on involving longitudinal motions of an aircraft. Theoretical methods involving the Laplace transformation and the procedures of nonlinear mechanics have been presented along with electrical-analog results for the responses of a canard aircraft to step control deflections and to the influence of two types of proportional automatic control.

著录项

  • 作者

    HOWARD J. CUREMAN;

  • 作者单位
  • 年度 1951
  • 页码 1-25
  • 总页数 25
  • 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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