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Servo-elasticity test of an aircraft with the flight control system

  • Junjie Zhang
  • , Chao Yang*
  • *此作品的通讯作者
  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

In order to reveal the servo-elasticity stability nature of an aircraft equipped with a flight control system, some active-control-system/structural dynamics interaction tests have been performed. The test principle and test method were described. Some typical test results were presented and compared with the calculated results, showing that the test method is reasonable.

源语言英语
页(从-至)998-1000
页数3
期刊Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
29
11
出版状态已出版 - 11月 2003

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