Li Huifeng, Ge Yajie, Li Zhaoyinget al. Adaptive BTT terminal guidance law for hypervelocity vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 569-573. (in Chinese)
Citation: Li Huifeng, Ge Yajie, Li Zhaoyinget al. Adaptive BTT terminal guidance law for hypervelocity vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 569-573. (in Chinese)

Adaptive BTT terminal guidance law for hypervelocity vehicle

  • Received Date: 10 May 2012
  • Rev Recd Date: 07 May 2013
  • Publish Date: 31 May 2013
  • An adaptive proportional navigation guidance law is proposed for hypersonic vehicle terminal guidance. The vehicle could be guided to impact the target precisely in a specific direction with required circular error probable. Based on the analysis of longitudinal flight, a convergence strategy was designed to make the proportional navigation guidance works earlier. The strategy allowed more time for the vehicle to meet the heading constraints at the impact. The precision of impact was affected by guidance parameters directly. However, vehicle would not conduct guidance commands ideally because of dynamic constraints. A close-loop nonlinear adaptive law was introduced to update guidance parameters online to improve the impact precision. Simulation results demonstrate the affectivity and accuracy of the proposed method.

     

  • [1]
    Kim B S,Lee J G,Han H S.Biased PNG law for impact with angular constraint[J].IEEE Transactions on Aerospace and Electronic Systems,1998,34(1):277-288
    [2]
    宋建梅,张天桥.带末端落角约束的变结构导引律[J].弹道学报,2001,13(1):16-20
    Song Jianmei,Zhang Tianqiao.The passive homing missiles variable structure proportional navigation with terminal impact angular constraint[J].Journal of Ballistics,2001,13(1):16-20(in Chinese)
    [3]
    Song T L,Shin S J,Cho H.Impact angle control for planar engagement[J].IEEE Transactions on Aerospace and Electronic Systems,1999,35(4):1439-1444
    [4]
    朱战霞,王建培.一种攻击地面固定目标的变系数比例导引律[J].飞行力学,2000,18(4):46-49
    Zhu Zhanxia,Wang Jianpei.A gain variable proportional guidance law for stationary target[J].Flight Dynamics,2000, 18(4):46-49(in Chinese)
    [5]
    Lu P.Intercept of nonmoving targets at arbitrary time-varying velocity[J].Journal of Guidance,Control,and Dynamics,1998, 21(1):176-178
    [6]
    Ulybyshev Y.Terminal guidance law based on proportional navigation[J].Journal of Guidance,Control,and Dynamics,2005,28(4):821-824
    [7]
    Lu P.Adaptive terminal guidance for hypervelocity impact in specified direction[J].Journal of Guidance,Control,and Dynamics,2006,29(2):269-278
    [8]
    Undurti A.Optimal trajectories for maneuvering reentry vehicles[D].Massachusetts Avenue,Cambridge,MA:Massachusetts Institute of Technology,2007
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