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变推力轴线无人机的建模与机敏性分析
引用本文:黄国勇,甄子洋,王道波.变推力轴线无人机的建模与机敏性分析[J].南京航空航天大学学报,2010,42(2).
作者姓名:黄国勇  甄子洋  王道波
作者单位:南京航空航天大学自动化学院,南京,210016
基金项目:国家自然科学基金,江苏省普通高校研究生科研创新计划,南京航空航天大学博士学位论文创新与创优基金 
摘    要:建立了与普通无人机相区别的变推力轴线无人机的全量教学模型.通过理论分析可知,变推力轴线技术的引入可以改善无人机的机动性和敏捷性.设计了气动舵面控制和推力变向控制相结合的无人机纵向姿态混合控制器,并对非线性模型描述的无人机进行了控制仿真,结果验证了混合控制策略的优越性,也体现了变推力轴线无人机具有比普通无人机更好的机敏性.

关 键 词:无人机  数学模型  姿态控制  飞行控制

Modeling and Smart Property Analyses of Variable Thrust Axis Based UAV
Abstract:A general model of a variable thrust axis based unmanned aerial vehicle (UAV) is built and it is different from the common UAV. According to the theory analysis, the introduction of the variable thrust axis technique can improve the maneuverability and the agility of UAV. A hybrid longitudinal attitude controller is designed by combining the aerodynamic rudder control and the variable thrust axis control, and the control of the described nonlinear model based UAV is simulated. Simulation results show the superiority of the hybrid control strategy. The variable thrust axis based UAV has better smart properties compared with the common UAV.
Keywords:unmanned aerial vehicle  mathematical model  attitude control  flight control
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