In response to the ever increasing accuracies in inertial navigation systems, the U. S. Air Force must develop higher accuracy reference systems. These reference systems must also be small enough to be utilized in the testing of navigation systems onboard fighter aircraft. One such proposed system utilizes carrier-phase Global Positioning System (CPGPS) transmitters mounted on MM-9 pods with receivers on the ground. This research examines one possible method of utilizing this system to determine the attitude and position of the aircraft, given position estimates for the transmitter's locations. The transmitter positioning algorithm showed that the geometry will be problematic for this configuration. However, if given the estimates of transmitter positions within the desired accuracy, the aircraft attitude and position algorithms worked effectively.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Wing Flexure Compensation for Aircraft Attitude and Position Determination in an Inverted Carrier-Phase Positioning System


    Beteiligte:
    B. W. Mahlum (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    103 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Aircraft attitude controller and wing system

    ALEXIS ANTHONY LIBERSON | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT ATTITUDE CONTROLLER AND WING SYSTEM

    LIBERSON ALEXIS ANTHONY | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft attitude controller and wing system

    Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT ATTITUDE CONTROLLER AND WING SYSTEM

    LIBERSON ALEXIS ANTHONY | Europäisches Patentamt | 2024

    Freier Zugriff