期刊文献+

基于遥测数据的无人机飞行包线估算方法研究

Study on UAV's flight envelope estimation method based on telemetry data
原文传递
导出
摘要 飞行包线对于无人机的飞行安全至关重要。为了建立更加完善的飞行包线,提出了一种基于遥测数据的气动参数辨识方法结合可达集理论的包线估计综合方法;基于动力学方程建立无人机的气动参数模型,利用辨识模型的参数解算不同高度下的飞行包线,再利用线性系统理论与可达集理论扩展计算不同飞行包线下的相关极限飞行参数;最后,基于某型无人机实际飞行中记录的遥测数据,解算了该无人机的飞行包线,验证了该方法的可行性和有效性。 The flight envelope is of primary importance to the UAV’s flight safety.To get more complete flight envelope,this paper puts forward a comprehensive method based on the telemetry data,combining aerodynamic parameter identification and reachability analysis.The aerodynamic parameter model of UAV is built on the basis of dynamic equation,and the flight envelopes at different heights are calculated by using the model parameters,and then the limit flight parameters in different flight envelopes are calculated by using the reachable analysis.At last,based on the telemetry data recorded in the actual flight of a UAV,this paper presents the flight envelope calculated by the comprehensive method and verifies the feasibility of the method.
作者 羊雨璇 高占宝 李绪隆 李宝安 YANG Yu-xuan;GAO Zhan-bao;LI Xu-long;LI Bao-an(School of Automation Science and Electrical Engineering,BUAA,Beijing 100191,China)
出处 《飞行力学》 CSCD 北大核心 2019年第1期1-5,共5页 Flight Dynamics
关键词 动力学方程 遥测数据 飞行包线 辨识模型 可达集理论 dynamic equation telemetry data flight envelope identification model reachability analysis
  • 相关文献

参考文献4

二级参考文献35

  • 1Zhu J J. Nonlinear tracking and decoopling by trajectory linearization [ R]. NASA Marshall Space Flight Center,1998.
  • 2Bevacqua T,Best E, Huizenga A,et al. Improved trajectory linearization flight controller for reusable launch vehicles [ R ]. AIAA 2004-875,2004.
  • 3Zhu J J. PD-spectral theory for multivariable linear time-varying systems [ C ] //Peshkin M. Proceeding of the 36th Conference on Decision & Control. San Diego: IEEE Control Systems Society, 1997:3908 - 3913.
  • 4Yang Lingyu,Shen Gongzhang. A new optimal control allocation method for aircraft with multiple control effectors [ R]. AIAA 2007-1052,2007.
  • 5杨凌宇,钟友武,申功璋.多操纵面飞机控制分配的非线性闭环迭代结构[C]//程代展,吴敏.第26届中国控制会议论文集(第四册).北京:北京航空航天大学出版社,2007:755-757.
  • 6Brinker J S, Wise K A. Flight testing of a reconfigurable flight control law on the X-36 tailless fighter aircraft [ R ]. AIAA-2000- 3941,2000.
  • 7Bennani S,Sluis R,Schram G, et al. Control law reconfiguration using robust linear parameter varying control [ R ]. AIAA-99- 4137,1999.
  • 8Boskovic J D, Mehra R K. Robust fault-tolerant control design for aircraft under state-dependent disturbances [ R ]. AIAA 2003- 5490.2003.
  • 9Burken J J, Lu P, Wu Z L, et al. Two reconfigurable flight-control design methods: robust servomechanism and control allocation [ J]. Journal of Guidance, Control and Dynamics,2001,24(3 ) : 482 - 493.
  • 10Joosten D A ,Boom T J J, Lombaerts T J J. Computationally efficient use of MPC and dynamic inversion for reconfigurable flight control [ R], AIAA 2008-7431,2008.

共引文献15

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部