Nonlinear control of aircraft at high angles of attack

被引：0
|
作者：
Edro, JO [1 ]
Mansfield, BA [1 ]
机构：
[1] Univ Witwatersrand, Sch Mech Ind & Aeronaut Engn, Johannesburg, South Africa
来源：
2004 IEEE AFRICON: 7TH AFRICON CONFERENCE IN AFRICA, VOLS 1 AND 2: TECHNOLOGY INNOVATION | 2004年
关键词：
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
The detailed nonlinear flight model is presented including the effects of thrust vectoring. A daisy chain controller was implemented to allow the use of the thrust vectoring to augment the control of the aircraft. A nonlinear dynamic inversion controller was applied to the pitch acceleration longitudinal mode of the aircraft. Numerical simulation was carried out using existing flight data, which includes high angle of attack and poststall effects.
引用
收藏
页码：431 / 436
页数：6
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