The development of digital autopilots and integrated avionics systems, applicable to many classes of vehicles and missions, was undertaken by Sperry Flight Systems in the mid-sixties. The first application of the system was planned for automatic flight control in the U.S. supersonic transport; the termination of that program, however, thwarted any flight experience. The second application, which has additional navigation and energy management functions, is an airborne simulator of the space shuttle vehicle. The latter system underwent a series of successful flight tests in a CV-990 aircraft under contract with NASA. The third application, which has new electronic displays, air data computation, and time-constrained guidance (i.e., specified position and altitude at a specified time), is in the DOT/NASA STOLAND test program. The STOLAND system is described specifically in this paper.


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    Titel :

    Navigation, guidance, and control systems for V/STOL aircraft.


    Beteiligte:
    Osder, S. S. (Autor:in) / Rouse, W. E. (Autor:in) / Young, L. S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1973-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Integrated navigation systems for V/STOL aircraft

    Duguid, A.W. | Engineering Index Backfile | 1962


    4-D guidance of STOL aircraft

    CAPEN, E. | AIAA | 1971


    A flight investigation of a terminal area navigation and guidance concept for STOL aircraft

    Smith, D. W. / Neuman, F. / Watson, D. M. et al. | NTRS | 1976


    A flight investigation of a terminal area navigation and guidance concept for STOL aircraft

    Smith, D. W. / Neuman, F. / Watson, D. M. et al. | NTRS | 1974


    STOL/VTOL Aircraft Characteristics, Terminal Navigation and Air Traffic Control

    Brandewie, D. Michael / Barriage, Joan B. | SAE Technical Papers | 1968