Since the traditional parabola trajectory is prone to be head off, wavy trajectory has the flight characteristics of defense penetration ability and increasing range. On the basis of flight characteristics of wavy trajectory missile, a method for flight program angle was designed. A specific formula was given. An optimization model was established. A conjugate gradient optimizing algorithm was used to solve the model and the result is compared with the former trajectory. It shows that optimized wavy trajectory can prove the feasibility of increasing range and valid defense penetration ability.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A Conjugate Gradient Optimization Algorithm for Wavy Trajectory of Missile



    Erschienen in:

    Applied Mechanics and Materials ; 427-429 ; 1368-1371


    Erscheinungsdatum :

    2013-09-27


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Missile trajectory optimization using a modified ant colony algorithm

    Kiyak, Zachary J. / Hartfield, Roy J. / Ledlow, Timothy W. | IEEE | 2014


    Generalized gradient algorithm for trajectory optimization

    ZHAO, YIYUAN / BRYSON, A. E. / SLATTERY, R. | AIAA | 1990


    Generalized gradient algorithm for trajectory optimization

    Zhao, Yiyuan / Bryson, A. E. / Slattery, R. | NTRS | 1990


    Missile trajectory optimization with agility issues

    Nasuti, Francesco / Innocenti, Mario | AIAA | 1996


    Simulated Annealing for Missile Trajectory Planning and Multidisciplinary Missile Design Optimization

    Tekinalp, O. / Utalay, S. / AIAA | British Library Conference Proceedings | 2000