HIDEC, a NASA sponsored program to develop and flight demonstrate integrated flight propulsion control modes on a McDonnell Douglas F-15 Eagle aircraft, is underway. Two high payoff integrated modes are being developed. The Trajectory Control/Energy Management mode will not only demonstrate increased weapon system effectiveness through fuel savings and increased intercept ranges, but will also serve as a stepping stone to other trajectory control applications such as terrain following-terrain avoidance and automated air combat. The Variable Operating Line mode will demonstrate benefits of increased thrust without increasing engine size and weight. The flight control and engine control modifications made to implement these modes will also support future NASA programs for optimizing flight propulsion control interactions.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Integrated flight/propulsion control: HIDEC modes


    Additional title:

    Integrierte Flug/Vortriebssteuerung. HIDEC-Betriebsarten


    Contributors:
    Yonke, W.A. (author) / Landy, R.J. (author) / Cushing, J.M. (author)


    Publication date :

    1984


    Size :

    7 Seiten, 16 Bilder, 4 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    VLF Integrated Flight/Propulsion Control

    Ostroff, H. H. | SAE Technical Papers | 1976


    Propulsion control specifications in integrated flight propulsion control systems

    ROCK, STEPHEN / EMAMI-NAEINI, ABBAS / ANEX, ROBERT | AIAA | 1988


    Integrated flight/propulsion control for helicopters

    Rock, Stephen M. / Neighbors, Ken | NTRS | 1994


    Integrated flight/propulsion control for helicopters

    Rock, S.M. / Neighbors, K. | Tema Archive | 1994