Rotating Spacecrafts can provide artificial gravity for long-term space missions, but the design of a Guidance and Control scheme for these vehicles is nuanced. For a three-segment vehicle with the propulsion element located at the center of mass, the vehicle must stabilize itself about this point even in the event of various off-nominal circumstances. Thus, a robust and passive spin stabilization system is needed. In this paper, various methods for stabilizing the system to allow for the exchange of mass and air between elements are explored and simulated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Passive Stabilization of Rotating Tethered Spacecraft


    Beteiligte:

    Kongress:

    AAS/AIAA Astrodynamics Specialist Conference ; 2023 ; Big Sky, MT, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Passive Stabilization of Rotating Tethered Spacecraft

    M. M. Wittal / S. M. Tavarez-Garcia | NTIS | 2023


    Passive Stabilization of Rotating Spacecraft Using Dynamic Fluid-Pressure Equilibrium

    Matthew M. Wittal / Taylor A. Peterson / Sara M. Tavarez-Garcia et al. | NTRS


    Passive Stabilization of Rotating Spacecraft Using Dynamic Fluid-Pressure Equilibrium

    M. M. Wittal / T. A. Peterson / S. M. Tavarez-Garcia et al. | NTIS | 2023


    Trajectory design, feedforward, and feedback stabilization of tethered spacecraft retrieval

    FLEURISSON, ERIC J. / VON FLOTOW / ANDREAS H. et al. | AIAA | 1993