Modeling and Simulation of Lazy Eight Aircraft Maneuver

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 ate 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.

关键词： Flight dynamics Flight simulation Control law PID controller Lazy Eight

作者: Pan Wenjun Liu Xing-Yu Wang Lixin

作者单位: School of Aeronautic Science and Engineering Beijing University of Aeronautics and Astronautics Beij General Configuration and Aerodynamics Department of Shanghai Aircraft Design and Research Institute

会议类型: 国际会议

会议名称: 2012 2nd International Conference on Computer Application and System Modeling(2012第二届计算机应用与系统建模国际会议)(ICCASM-2012)

会议地点: 沈阳

会议语种:英文

页码: 935-938

在线出版日期: 2012-07-27（万方平台首次上网日期，不代表论文的发表时间）