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一种基于动态逆的控制方案在无人机中的应用研究
引用本文:苏丙未,万胜,陈欣,杨一栋.一种基于动态逆的控制方案在无人机中的应用研究[J].南京航空航天大学学报,2000,32(6):706-710.
作者姓名:苏丙未  万胜  陈欣  杨一栋
作者单位:南京航空航天大学自动控制系南京,210016
摘    要:动态逆技术通过成功的实际飞行测试而获得广泛认同,目前该研究热点在于对象模型的不确定性的抑制及鲁棒性的研究。文中提出一种基于在线神经网络的新型动态逆控制器,其主要思想是通过在线迭代的神经网络最大程度地挖无人机非线性不确定模型及其逆模型,同时通过一个梯度修正环节来补偿误差的影响。仿真验证包括三部分:对极快变量回路的仿真、航迹角跟随的仿真以及三维空间中对给定轨迹的跟踪。仿真结果表明,该方案能够解决精确的

关 键 词:无人机  动态逆  神经网络  飞行控制系统
修稿时间:1999年11月8日

Dynamic Inversion Based Control Scheme Applied to Pilotless Aircraft
Su Bingwei,Wan Sheng,Chen Xin,Yang Yidong.Dynamic Inversion Based Control Scheme Applied to Pilotless Aircraft[J].Journal of Nanjing University of Aeronautics & Astronautics,2000,32(6):706-710.
Authors:Su Bingwei  Wan Sheng  Chen Xin  Yang Yidong
Abstract:While the field involving pilotless aircraft is increasingly widening, challenge is also existing in the flight control system. The dynamic inversion technique is approved by kinds of flight tests recently. Now the research focus of this method lies in the compensation of the effect on the model uncertainty and the robustness. A new dynamic inversion controller based on online neural networks is presented and verified by a precise 3-D path following problem. The key idea of the method is that a modified unit by gradient method is used to compensate the error while using online neural networks to form dynamic inversion controller. The advantage of the method is that the converzence can be achieved even the error is large. This is that because both the online neural network inversion controller and the gradient modified unit may elimiate the error at the same time.
Keywords:pilotless aircraft  flight control system  dynamic inversion  neural network  uncertainty
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