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基于直线-圆弧混合导引的无人机自主返航控制技术 被引量:1

Autonomous Return Control Technology of UAV Based on Linear-arc Hybrid Guidance
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摘要 应急返航是无人机飞行过程中的一种紧急处置措施,返航初始条件的不确定性对无人机的自主控制能力提出了很高的要求。文中以无人机应急返航的需求为牵引,给出了一种基于Dubins算法的路径在线规划方法,并提出了一种基于直线-圆弧混合引导的复杂路径高精度跟踪控制方法。通过六自由度仿真,验证了路径规划的正确性及轨迹跟踪的精度,并通过蒙特卡洛仿真,进一步验证了本控制方案的逻辑完整性。本方案在工程应用中具有一定的借鉴意义。 Emergency return is an emergency treatment during the flight of the UAV.The uncertainty of the initial conditions of the return flight puts high demands on the autonomous control capability of the UAV.In this paper,based on the demand of UAV emergency return,a path online planning method based on dubins algorithm is presented,and a high-precision tracking control method based on linear-arc hybrid guidance is proposed.The six-degree-of-freedom simulation is used to verify the correctness of the path planning and the accuracy of the trajectory tracking.The Monte Carlo simulation is used to further verify the logical integrity of the control scheme.This scheme has certain reference significance in engineering application.
作者 刘茂汉 徐芳芳 LIU Maohan;XU Fangfang(Shenyang Aircraft Design&Research Institute,Shenyang 110035,China)
出处 《飞机设计》 2019年第4期5-8,共4页 Aircraft Design
关键词 圆弧导引 自主返航 航线规划 控制律 仿真 arc guidance autonomous return route planning control law simulation
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  • 1吴春英,卢京潮,屈耀红,田琪.基于LQR技术的无人机纵向控制律设计[J].飞行力学,2006,24(3):33-36. 被引量:6
  • 2张明廉主编.飞行控制系统[M]. 航空工业出版社, 1994
  • 3Georgea P.Fiber Optic Gyro Evolution Concept to Product[].AIAA GuidanceNavigation and Control Conference.1992
  • 4Joseph B Mueller,Michael APaluszek,Yiyuan Zhao.Development of an Aerodynamic Model and Control Law Design for a High Altitude Airship[].AIAA rd Unmanned Unlimited Technical Conference Workshop and Exhibit.2004
  • 5Sadraey M,Colgren R.Two DOF robust nonlinear autopilotdesign for a small UAV using a combination of dynamicinversion and loop shaping[].AIAA Guidance Naviga-tion and Control Conference.2005
  • 6K.Wise.A Bank-To-Turn Missile Autopilot Design Approach Using LQG/LTR Control Theory[].AIAA th Aerospace Sciences Meeting.1988
  • 7K.Wise.Bank-to-Turn Missile Autopilot Design Using Loop Transfer Recovery[].AIAA th Aerospace Sciences Meeti ng.1988
  • 8Menon P K,Vaddi S S,Sengupta P.Robust landing guidance law for impaired aircraft[J].Journal of Guidance,Control,and Dynamics,2012,35(6):1865-1877.
  • 9Rolf R,Anthony C.Fault tolerant flight control via adaptive neural network augmentation[C]// Proc.of the Guidance,Na- vigation,and Control Conference and Exhibit,1998:20-34.
  • 10Tandale M,Valasek J.Fault-tolerant structured adaptive model inversion control[J].Journal of Guidance,Control,and Dy- namics,2006,29(3):635-642.

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