The primary purpose of this study was to program and simulate advanced flight command computations for flight command functions common to many missions. A systems approach is taken in making use of available aircraft sensors and/or radio information to accomplish mission objectives. The functions simulated were horizontal (area) navigation, horizontal steering, vertical navigation, pitch control, energy maneuverability (optimum climb), and automatic throttle. Both completely automatic flight and manual (display) steering were simulated. The simulation was conducted at the hybrid computation facilities of the Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, Ohio. The aircraft characteristics used were those of the F-4C. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Definition and Analysis of Flight Command Functions and Computations

    A. S. Marino / W. E. McAdam / R. C. Chojnacki | NTIS | 1968


    Study on Flight Command and Training Simulation System about Aircraft

    Hu, Chao Jiang ;Liu, Chang Wei ;Ma, Qiao Bing | Trans Tech Publications | 2012


    FLIGHT CONTROL SYSTEM COMMAND SELECTION

    MATSUI GEN | Europäisches Patentamt | 2020

    Freier Zugriff

    Command Limiting in Reconfigurable Flight Control

    Bodson, M. | Online Contents | 1998


    Command Limiting in Reconfigurable Flight Control

    Marc Bodson / William A. Pohlchuck | AIAA | 1998