General-purpose rigid-body six-degrees-of-freedom program is used to solve wide variety of atmospheric flight mechanics and orbital transfer problems. Written for analysis of powered or unpowered vehicles operation near rotating oblate planet, typical applications include: guidance and flight-control system simulation and analysis, loads and dispersion-type analysis.


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    Title :

    Optimizing simulated trajectories


    Contributors:

    Published in:

    Publication date :

    1978-03-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Optimizing Simulated Trajectories Of Rigid Bodies

    Brauer, Garry L. / Olson, David W. / Stevenson, Robert | NTRS | 1989


    Optimization Of Simulated Trajectories

    Brauer, Garry L. / Olson, David W. / Stevenson, Robert | NTRS | 1989


    Optimizing Steady Turns for Gliding Trajectories

    Di Donato, Pedro F. A | Online Contents | 2016


    Optimizing Trajectories for Suborbital Human Spaceflight

    Ryan Kobrick / David Spencer | AIAA | 2007


    Optimizing Steady Turns for Gliding Trajectories

    Di Donato, Pedro F. A. / Atkins, Ella M. | AIAA | 2016