A batch air combat simulation environment, the tactical maneuvering simulator (TMS), is presented. The TMS is a tool for developing and evaluating tactical maneuvering logics, but it can also be used to evaluate the tactical implications of perturbations to aircraft performance or supporting systems. The TMS can simulate air combat between any number of engagement participants, with practical limits imposed by computer memory and processing power. Aircraft are modeled using equations of motion, control laws, aerodynamics, and propulsive characteristics equivalent to those used in high-fidelity piloted simulations. Data bases representative of a modern high-performance aircraft with and without thrust-vectoring capability are included. To simplify the task of developing and implementing maneuvering logics in the TMS, an outer-loop control system, the tactical autopilot (TA), is implemented in the aircraft simulation model. The TA converts guidance commands by computerized maneuvering logics from desired angle of attack and wind-axis bank-angle inputs to the inner loop control augmentation system of the aircraft. The capabilities and operation of the TMS and the TA are described.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A high-fidelity, six-degree-of-freedom batch simulation environment for tactical guidance research and evaluation


    Beteiligte:

    Erscheinungsdatum :

    1993-07-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    An integrated environment for tactical guidance research and evaluation

    Goodrich, Kenneth H. / Mcmanus, John W. | NTRS | 1990




    Rotorcraft Tactical Simulation Modelling Fidelity Issues

    Salinas, A. Y. / Royal Aeronautical Society | British Library Conference Proceedings | 1994