The navigation and flight director guidance systems implemented in the NASA/FAA helicopter microwave landing system (MLS) curved approach flight test program is described. Flight test were conducted at the U.S. Navy's Crows Landing facility, using the NASA Ames UH-lH helicopter equipped with the V/STOLAND avionics system. The purpose of these tests was to investigate the feasibility of flying complex, curved and descending approaches to a landing using MLS flight director guidance. A description of the navigation aids used, the avionics system, cockpit instrumentation and on-board navigation equipment used for the flight test is provided. Three generic reference flight paths were developed and flown during the test. They were as follows: U-Turn, S-turn and Straight-In flight profiles. These profiles and their geometries are described in detail. A 3-cue flight director was implemented on the helicopter. A description of the formulation and implementation of the flight director laws is also presented. Performance data and analysis is presented for one pilot conducting the flight director approaches.


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    Titel :

    Navigation and Flight Director Guidance for the NASA/FAA Helicopter Mls Curved Approach Flight Test Program


    Beteiligte:
    A. V. Phatak (Autor:in) / M. G. Lee (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    133 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    NASA-FAA helicopter Microwave Landing System curved path flight test

    Swenson, H. N. / Hamlin, J. R. / Wilson, G. W. | NTRS | 1983


    NASA-FAA helicopter Microwave Landing System curved path flight test

    Swenson, H. N. / Hamlin, J. R. / Wilson, G. W. | NTRS | 1984


    Nasa-FAA Helicopter Microwave Landing System Curved Path Flight Test

    H. N. Swenson / J. R. Hamlin / G. W. Wilson | NTIS | 1983