Numerical comparison is made in idealized problem wherein computations are simple enough not to require machine computation; orthodox solution involving usual Lagrange multiplier associated with kinematical restraint, and unorthodox solution in which this multiplier is treated as identically zero; pertinence to problem of rocket trajectory.


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    Title :

    Approximations in flight optimization problems


    Additional title:

    Aerospace Eng


    Contributors:

    Published in:

    Publication date :

    1961


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English