Description of self-contained aids which fall into two groups, air data and Doppler radar; inertial navigation combines constant direction-seeking properties of gyroscope with accelerometers and integrators to provide navigation system with six major characteristics which are described; operational uses of inertial navigation systems and use of combined Doppler inertial systems are examined together with overall system aspects of complete navigation system. Article is based on paper presented before IATA Aircraft Navigation Conference, Miami, Fla 1965.


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    Title :

    Performance of inertial navigation equipment


    Additional title:

    Flight


    Contributors:

    Published in:

    Flight ; 89 , n 2971


    Publication date :

    1966


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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