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Original Articles

A Nonlinear Optimal Guidance Law with Terminal Impact Angle Constraint

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Pages 1319-1324 | Received 08 Jul 2011, Accepted 29 Nov 2011, Published online: 12 Mar 2012

References

  • Cloutier , J. R. State-Dependent Riccati Equation Techniques: An Overview . Proceedings of the American Control Conference . Edited by: Davis , C. G. and Yeh , R. T. pp. 932 – 936 . New-Mexico
  • Hu , S. S. , Wang , Z. Q. and Hu , W. L. , eds. 2005 . Optimal Control Theory and System , Beijing : Science Press .
  • Lu , P. , Doman , D. B. and Schierman , J. D. 2006 . Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction . Journal of Guidance, Control, and Dynamic , 29 ( 2 ) : 269 – 278 .
  • Wang , W. H. , Hou , Fuguo , Tan , Huachun and Bubb , H. 2010 . A Framework for Function Allocations in Intelligent Driver Interface Design for Comfort and Safety . International Journal of Computational Intelligence Systems , 5 : 531 – 541 .
  • Kim , M. and Grider , K. 1973 . Terminal guidance for impact att itude angle constrained flight trajectories . IEEE Transact ions on Aerospace and Electronic Systems , 9 ( 6 ) : 852 – 859 .
  • Idan , M. , Golan , O. M. and Guelman , M. 1995 . Optimal planar interception witht erminal constraints . Journal of Guidance, Control and Dynamics , 18 ( 6 ) : 1273 – 1279 .
  • Lee , Y. , Ryoo , C. and Kim , E. Optimal guidance with constraints on impact angle and terminal acceleration . AIAA Guidance, Navigation, Control Conference . Austin , , USA
  • Ryoo , C. K. , Cho , H. J. and Tahk , M. J. 2006 . Time to go weighted optimal guidance with impact angle constraints . IEEE Transactions on Control Systems Technology , 14 ( 3 ) : 483 – 492 .
  • Manchester , I. R. and Savkin , A. V. 2003 . Circular navigation missile guidance with incomplete information and uncertainty, AIAA-2003-5448
  • Mao , X. , Yang , S. and Xu , Y. 2007 . Coning Motion Stability of Wrap Around Fin Rockets . Science in China Series E: Technological Sciences , 50 ( 3 ) : 343 – 350 .
  • Yan , X. , Yang , S. and Zhang , C. 2010 . Coning Motion of Spinning Missiles Induced by the Rate Loop . Journal of Guidance, Control, and Dynamics , 33 ( 5 ) : 1490 – 1499 .
  • Zipfel , P. H. 2000 . Modeling and Simulation of Aerospace Vehicle Dynamics , AIAA Education Series .
  • George , M. S. 2004 . Missile Guidance and Control Systems , New York : Springer–Verlag .
  • Qian , X. , Lin , R. and Zhao , Y. 2003 . Missile Flight Mechanics , Beijing : Beijing Institute of Technology Publishing House .
  • Garnell , P. 1980 . Guided Weapon Control Systems , 2nd ed. , New York : Pergamon .

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