Hardware and software were developed for the data evaluation of a flight measurement system consisting of inertial sensors on board the aircraft and ground-based flight path measurement stations. The results obtained are reference data for flight path, velocity, attitude angles and gyro drift. External measurements such as radar, cinetheodolites or TACAN, together with inertial data recorded in the aircraft, are evaluated by optimum smoothing techniques. Flight test results are presented.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Flight Testing of Inertial Navigation Systems: Hardware and Software Description


    Contributors:
    W. Lechner (author) / H. J. Hotop (author) / H. P. Zenz (author)

    Publication date :

    1983


    Size :

    93 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Inertial Navigation Systems Testing Handbooks

    L. D. Plews / C. W. Brinkley / K. E. Reeser | NTIS | 1976



    Flight Testing Navigation Systems

    Biezad, Daniel J. | AIAA | 1999



    Flight evaluation of differential GPS aided inertial navigation systems

    Mcnally, B. David / Paielli, Russell A. / Bach, Ralph E., Jr. et al. | NTRS | 1992