Journal of Projectiles, Rockets, Missiles and Guidance >
The Design of Adaptive Prediction Control Law of Miniature Duct Fan UAV
Received date: 2011-03-26
Online published: 2025-05-30
In order to solve the problem of model uncertainty and non-asymptotic stability of the system, an improved control law of the miniature duct fan UAV attitude prediction was designed by combining the prediction control method and simple adaptive control method. The simulation results indicate that the control law makes the UAV's attitude outputs follow the input signals rapidly, and the coupling interaction between control channels is eliminated. When the parameters of the object model changes, dynamic matrix control (DMC) prediction controller is still valid. The control law is robust.
Key words： dynamic matrix control; duct fan UAV; model conference; adaptive
XU Min , FAN Ningjun , WU Yanxuan , WANG Zhengjie . The Design of Adaptive Prediction Control Law of Miniature Duct Fan UAV[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(6) : 51 -54 . DOI: 10.15892/j.cnki.djzdxb.2011.06.022
| [1] | 席裕庚. 预测控制[M]. 北京: 国防工业出版社, 1993. |
| [2] | Sobel K, Kaufman H, Mabius L. Implicit adaptive control for a class of MIMO systems[J]. IEEE Transactions on Aerospace, 1982, 18(5): 576-590. |
| [3] | BARKANA I. Simple adaptive control for non-minimum phase autopilot design[C]// AIAA Guidance, Navigation, and Control Conference and Exhibit, Providence R I, USA, 2004. |
| [4] | WD MORSE. Model following reconfigurable flight control system for the AFTI F-16[J]. Journal of Guidance Con-trol and Dynamics, 1990, 13(6): 969-976. |
| [5] | H Chen, F Allgower. A Quasi-Infinite horizon nonlinear model predictive control schemes with guaranteed stability[J]. Automatica, 1998, 34(10): 1205-1217. |
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