Abstract A method for simulating a flexible spacecraft motion using Lagrange’s quasivelocity formulation is considered. An algorithm of quasivelocity formation by Walsh’s means is proposed. This method can be used to evaluate a quasistatic microacceleration field component in the spacecraft internal environment.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Simulation of a flexible spacecraft motion to evaluate microaccelerations


    Contributors:

    Published in:

    Publication date :

    2009-12-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Simulation of a flexible spacecraft motion to evaluate microaccelerations

    Sedel’nikov, A. V. / Serpukhova, A. A. | Online Contents | 2009


    The problem of estimating microaccelerations aboard Foton-M4 spacecraft

    Anshakov, G. P. / Belousov, A. I. / Sedel’nikov, A. V. | Springer Verlag | 2017


    The problem of estimating microaccelerations aboard Foton-M4 spacecraft

    Anshakov, G. P. / Belousov, A. I. / Sedel’nikov, A. V. | Online Contents | 2017


    The problem of ensuring requirements for microaccelerations on board of small spacecraft

    A. V. Sedelnikov / E. V. Eskina / A. S. Taneeva et al. | DOAJ | 2022

    Free access

    Compensating Microaccelerations from a Temperature Shock

    Sedelnikov, Andry / Salmin, Vadim / Lazarev, Yuri et al. | Springer Verlag | 2021