摘要
给出了一种小型隐身性无人机的平面导航与控制方案。基于GPS/航路推算组合导航方法,文中利用Matlab的SimuLink工具箱建立了无人机六自由度模型,设计了相应的水平控制与导航方案,给出了一种风场估计方法以及风场下的航迹修正方案,并针对某具有隐身功能的无人机进行了导航控制律设计,最终的仿真结果验证了该组合导航方法以及相应制导律的可靠性和实用性。
A method of horizontal navigation and control for mini remotely piloted vehicles is proposed. Based on GPS/ DR（dead reckoning） integrated navigation system, the model of UAV was built using SimuLink toolbox of Matlab, a method of horizontal navigation and control is studied, and the design of navigation control law on same mini-RPV was presented. The final simulation results validate the reliability and feasibility of this method.
出处
《弹箭与制导学报》
CSCD
北大核心
2007年第4期16-18,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
组合导航
无人机
全球定位系统(GPS)
航路推算
dead reckoning
remotely piloted vehicles
global positioning system
integrated navigation
