• Electronics Optics & Control
  • Vol. 24, Issue 8, 5 (2017)
FU Zhu-mu, ZHAO Chen-dong, and SUN Xing-long
Author Affiliations
  • [in Chinese]
  • show less
    DOI: 10.3969/j.issn.1671-637x.2017.08.002 Cite this Article
    FU Zhu-mu, ZHAO Chen-dong, SUN Xing-long. Integrated Optimal Control Law Design for Missile Guidance and Control with Terminal Impact Angle Constraint[J]. Electronics Optics & Control, 2017, 24(8): 5 Copy Citation Text show less
    References

    [5] LIN C F, WANG Q, SPEYER J L, et al.Integrated estimation, guidance, and control system design using game theoretic approach[C]//Proceedings of American Control Conference, American Automatic Control Council,Evanston,IL, 1992: 3220-3224.

    [6] LIN C F, BIBEL J E, OHLMEYER E, et al.Optimal design of integrated missile guidance and control[C]//Proceedings of the World Aviation Conference, Anaheim, CA, 1998.doi: 10.2514/6.1998-5519.

    [7] SERRANI A, ZINNECKER A M, FIORENTINI L, et al.Integrated adaptive guidance and control of constrained nonlinear air-breathing hypersonic vehicle models[C]//Proceedings of the American Control Conference, Mis-souri, USA:IEEE, 2009:3172-3177.

    FU Zhu-mu, ZHAO Chen-dong, SUN Xing-long. Integrated Optimal Control Law Design for Missile Guidance and Control with Terminal Impact Angle Constraint[J]. Electronics Optics & Control, 2017, 24(8): 5
    Download Citation