The focus of this control has been to develop the control technology required to identify the sophistication required for the Aeroassisted Orbital Transfer Vehicle (AOTV) control system. An angle of attack, bank angle command control technique has been developed which uses either on-off thruster or proportional thruster. An angle of attack adaptive controller was included to minimize the reactor control system (RCS) usage due to payload center of gravity uncertainties. The guidance and control techniques were verified using a detail six degrees-of-freedom simulation. Mission sensitivity was developed for uncertainties in the entry state, mass properties, atmosphere, aerodynamic, and sensor.


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    Titel :

    Aeroassisted Orbital Transfer Vehicle Control Technology


    Beteiligte:

    Erscheinungsdatum :

    1988


    Format / Umfang :

    136 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Aeroassisted orbital transfer mission evaluation

    LETTS, W. / PELEKANOS, A. | AIAA | 1982



    Optimal trajectories for aeroassisted orbital transfer

    Miele, A. / Venkataraman, P. | Elsevier | 1984