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Modeling and simulation of lazy eight aircraft maneuver

  • Wenjun Pan*
  • , Lixin Wang
  • , Xing Yu Liu
  • *此作品的通讯作者
  • Beihang University
  • Shanghai Aircraft Design and Research Institute

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

The Lazy Eight aircraft maneuver is researched through numerical simulation. First, a six DOF aircraft flight dynamics model is developed. To control the aircraft performing the maneuver, a basic flight control law is designed, employing classical PID controllers in both pitch and roll loop. Commands for maneuver simulation are derived from the descriptions of Lazy Eight maneuver flight procedure. By proper settings of the commands and PID controllers' gain values, Lazy Eight maneuver simulation is conducted exactly according to the maneuver descriptions. The model established in paper also provides researchers and a method to simulate other aircraft maneuvers.

源语言英语
主期刊名Proceedings of the 2012 International Conference on Computer Application and System Modeling, ICCASM 2012
935-938
页数4
出版状态已出版 - 2012
活动2012 2nd International Conference on Computer Application and System Modeling, ICCASM 2012 - Shenyang, 中国
期限: 27 7月 201229 7月 2012

出版系列

姓名Proceedings of the 2012 International Conference on Computer Application and System Modeling, ICCASM 2012

会议

会议2012 2nd International Conference on Computer Application and System Modeling, ICCASM 2012
国家/地区中国
Shenyang
时期27/07/1229/07/12

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