Airplane control law which ensures minimum fuel consumption; relation between well-known minimum flight-time problem when controlling airplane in variable wind conditions and minimum fuel-consumption problems during given flight time is considered; solution of minimum fuel-consumption problem under simultaneous control of flight angle and of engine power level as well as under control of only operating mode of engine is given. (see also English translation in Automation and Remote Control n 11 Nov 1967 p 1781-4) (For Translation See Automation and Remote Control)


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    Title :

    O zakone upravleniya samoletom, obespechivayushchem minimum raskhoda topliva


    Additional title:

    O zakone upravleniya samoletom, obespechivayushchem minimum raskhoda topliva


    Contributors:

    Published in:

    Publication date :

    1967


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English