Lateral Acceleration Control of Aircraft Using PID, Linear Quadratic Regulator (LQR) and Linear Quadratic Integral (LQI); a Comparative Case Study

被引：0
作者：
ul Hasan, Ehtisham [1 ]
Khan, Amna [1 ]
Abbasi, Afaq Ahmed [2 ]
机构：
[1] Air Univ, Dept Mechatron Engn, Islamabad, Pakistan
[2] Northwestern Polytech Univ, Dept Fluid Mech, Xian, Shaanxi, Peoples R China
来源：
2018 5TH INTERNATIONAL CONFERENCE ON ELECTRICAL AND ELECTRONIC ENGINEERING (ICEEE) | 2018年
关键词：
side slip; lateral acceleration; hydro-mechanically; electrically; PID; LQR; LQI;
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：
Maneuverability is one of the key factors associated with fighter aircrafts. Effect of side slip in the form of lateral acceleration can significantly affect the stability of aircraft during maneuvers like coordination and therefore, must be addressed hydro-mechanically or electrically on aircrafts. Aircraft lateral acceleration models have been developed and control is implemented using Proportional integral Derivative-PID, Linear Quadratic Regulator-LQR and Linear Quadratic Integral-LQI. The responses of three are shown and compared. Results appreciate effectiveness of modern control techniques in contrast to classical control.
引用
收藏
页码：173 / 177
页数：5
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