期刊文献+

A hybrid guidance law of LOS acceleration feedback for missile against maneuvering targets

原文传递
导出
摘要 A quantised backstepping robust guidance law of three-dimension(3-D)space for compound control of reaction control jets and aerodynamic surfaces is proposed to attenuate the unknown target manoeuvre in this paper.The presented guidance law guarantees that the rates of line of sight converge to a residual circle centred at the origin whose radius is depended on the target manoeuvres,quantised length and guidance law gains.The simulations are given to illustrate the effectiveness of the proposed guidance law.
出处 《Journal of Control and Decision》 EI 2017年第3期168-178,共11页 控制与决策学报(英文)
基金 National Science Foundation of China[grant number 61673050] Aeronautical Science Foundation of China[grant number 201401M5001] Open Research Project of the State Key Laboratory of Industrial Control Technology,Zhejiang University,China[grant number ICT1600229].
  • 相关文献

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