Research on aerobraking guidance schemes is presented. The intent is to produce aerobraking guidance trajectories exhibiting many of the desirable characteristics of optimal aerobraking trajectories. Both one-control schemes and two-control schemes are studied. The research is in the interest of aeroassisted flight experiment vehicles (AFE) and aeroassisted orbital transfer (AOT) vehicles.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Guidance Trajectories for Aeroassisted Orbital Transfer


    Contributors:
    A. Miele (author)

    Publication date :

    1990


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English