Li Yanhui, Li Ming, Zhou Ling, Zhang Nan. UAV flight controller design method based on model matching used for electro-optical reconnaissance[J]. Infrared and Laser Engineering, 2015, 44(2): 693-698.
| Citation:
|
Li Yanhui, Li Ming, Zhou Ling, Zhang Nan. UAV flight controller design method based on model matching used for electro-optical reconnaissance[J]. Infrared and Laser Engineering, 2015, 44(2): 693-698.
|
UAV flight controller design method based on model matching used for electro-optical reconnaissance
- 1.
Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China
- Received Date: 2014-06-11
- Rev Recd Date:
2014-07-13
- Publish Date:
2015-02-25
-
Abstract
The application of UAV in the field of electro-optical reconnaissance is more and more widely. Desining a robust flight controller for UAV is an essential technique. A flight controller design method based on model matching and genetic algorithm optimization was proposed in this paper. A nonlinear model was used as the controlled object of this method. Compared with the classic flight controller design method, this method could access the needed controllers quickly and conveniently. A nonlinear mathematical six-degree-of-freedom model of a UAV was established, the aerodynamics, engine and environmental model were all included in this model. Using the above method, a UAV flight controller was designed. Based the finite state machine theory, the flight management model was established to design flight modes and carry out the controller switch. Finally, the six degrees of freedom nonlinear simulation was carried out to verify the effectiveness of the designed controller.
-
References
|
[1]
|
Lou Shuli. UAV electro-optical reconnaissance and surveillance technology [J]. Infrared and Laser Engineering, 2006, 10: 120-121. (in Chinese) |
|
[2]
|
|
|
[3]
|
Wang Xiao, Yi Ming, Hong Ming. Application of UAV system in electro-optical countermeasure [J]. Infrared and Laser Engineering, 2006, 10: 122-125. (in Chinese) |
|
[4]
|
|
|
[5]
|
Guo Suofeng, Shen Gongzhang. Advanced flight control system[M]. Beijing: National Defense Industry Press, 2003. (in Chinese) |
|
[6]
|
|
|
[7]
|
|
|
[8]
|
Wang Xiaoping, Cao Liming. Genetic Algorithm[M]. Xi'an: Xi'an Jiaotong University Press, 2005. (in Chinese) |
|
[9]
|
Pan Wei, Wang Xueyong, Jing Yuanwei. Mixed H2/H state feedback controllers based on genetic algorithm [J]. Control and Decision, 2005, 20(2): 132-136. (in Chinese). |
|
[10]
|
|
|
[11]
|
|
|
[12]
|
Li Guangwen. NGA based on uniform design and its application in optimization of FCS[J]. Acta Aeronautica ET Astronautica Sinica, 2008, 29: 73-78. (in Chinese) |
|
[13]
|
Wang Yong. Lateral deviation correction control for UAV taxiing[J]. Acta Aeronautica ET Astronautica Sinica, 2008, 29: 142-149. (in Chinese) |
|
[14]
|
|
|
[15]
|
Qian Xingfang, Lin Ruixiong, Zhao Yanan.Flight DynaIllic S0, Missile [M].Beijing: Beijing Institute of Technology Press,2000.(in Chinese) |
|
[16]
|
|
|
[17]
|
Li Ming. Hardware in closed loop simulation system for aircraft based on rapid simulation prototype [J]. Optics and Precision Engineering, 2008, 16: 1950-1955. (in Chinese) |
-
-
Proportional views
-
DownLoad: