Modeling and Simulation Analysis of a Kind of High Speed Aircraft

摘要：

　　High speed aircraft is researched widely by researchers because of its high value of application in the weapon design and military purpose.The modeling and simulation of high speed model is research and the open loop response is researched.At last,detailed numerical simulation was done with a real simplified pitch channel system model to testify the ability of aircraft body.

关键词： Disturbance Observer Backstepping Missile Control system

作者: Jing Li Hui Li Junwei Lei

作者单位: College of Weaponry engineering,Naval Engineering University,Wuhan,430000,China College of Coastal Defense,Naval Aviation University,Yantai,264001,China

会议类型: 国际会议

会议名称: 2019 International Seminar on Automation,Intelligence,Computing, and Networking (ISAICN 2019) (2019自动化、智能、计算和网络国际研讨会)

会议地点: 浙江宁波

会议语种:英文

页码: 347-351

在线出版日期: 2019-07-06（万方平台首次上网日期，不代表论文的发表时间）