The formulation and implementation of navigation systems used for research investigations in the V/STOLAND avionics system are described. The navigation systems prove position and velocity in a cartestian reference frame aligned with the runway. They use filtering techniques to combine the raw position data from navaids (e.g., TACAN, MLS) with data from onboard inertial sensors. The filtering techniques which use both complementary and Kalman filters, are described. The software for the navigation systems is also described.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Navigation systems for approach and landing of VTOL aircraft


    Beteiligte:
    Schmidt, S. F. (Autor:in) / Mohr, R. L. (Autor:in)

    Erscheinungsdatum :

    01.10.1979


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    AUTOLAND SYSTEM FOR VTOL AIRCRAFT, VTOL AIRCRAFT, AND LANDING CONTROL METHOD FOR VTOL AIRCRAFT

    KOJIMA TORU / MORI SATOSHI | Europäisches Patentamt | 2024

    Freier Zugriff

    Damping Landing Gear Systems for VTOL Aircraft

    MORRIS KEVIN / BRODEUR NICHOLAS / FLYNN-ROBITAILLE PASCAL | Europäisches Patentamt | 2021

    Freier Zugriff