In this paper the Monte-Carlo method was used to investigate the sounding rocket dispersion. It was assumed that the rocket is equipped with a control unit composed of 32 solid propellant lateral thrusters. The 6 degree-of-freedom model was developed and implemented in the MATLAB/Simulink environment. Several factors affecting the projectile dispersion were taken into account, including uncertainties in rocket’s inertial and aerodynamic parameters, magnitude and direction of wind velocity as well as uncertainties in initial conditions. In addition, the influence of the malfunction of the rocket fins and the time of flight of its occurrence on the mean impact point was investigated.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Analysis of Sounding Rocket Dispersion Using Monte-Carlo Simulation


    Weitere Titelangaben:

    Lect. Notes in Networks, Syst.


    Beteiligte:
    Szewczyk, Roman (Herausgeber:in) / Zieliński, Cezary (Herausgeber:in) / Kaliczyńska, Małgorzata (Herausgeber:in) / Bučinskas, Vytautas (Herausgeber:in) / Miedziński, Dariusz (Autor:in) / Głȩbocki, Robert (Autor:in) / Jacewicz, Mariusz (Autor:in)

    Kongress:

    Conference on Automation ; 2023 ; Warsaw, Poland March 07, 2023 - March 09, 2023



    Erscheinungsdatum :

    2023-02-05


    Format / Umfang :

    12 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Sounding Rocket

    J. T. Clarke | NTIS | 1998


    Sounding Rocket

    Clarke, John T. | NTRS | 1998


    Recent advances in the theory of sounding rocket dispersion analysis

    AMMONS, R. / HOULT, C. / SOLLOW, P. | AIAA | 1970