The crew emergency return vehicle (CERV) autoland feasibility study focused on determining the controllability of the NASA Langley high lift over drag CERV for performing an automatic landing at a prescribed runway. An autoland system was developed using integral linear quadratic Gaussian (LQG) design techniques. The design was verified using a nonlinear 6 DOF simulation. Simulation results demonstrate that the CERV configuration is a very flyable configuration for performing an autoland mission. Adequate stability and control was demonstrated for wind turbulence and wind shear. Control surface actuator requirements were developed.


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    Titel :

    Crew Emergency Return Vehicle Autoland Feasibility Study


    Beteiligte:
    J. A. Bossi (Autor:in) / M. A. Langehough (Autor:in) / K. L. Lee (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    168 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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