Traditional flying qualities metrics use first-order descriptors of the "classical- aircraft modes such as the phugoid, short-period, Dutch roll, etc. These modes are often difficult to distinguish from one another in modern aircraft for which the dynamics are usually coupled, leaving designers to develop lower-order equivalent systems as approximations to the behavior of the real aircraft. On the other hand, modern optimal or robust control techniques directly address multiple-input/multiple-output systems, with coupled dynamics, and they function well with higher-order measures of system behavior like state covariances or signal norms. This work presents a new method of approximating the traditional flying qualities requirements for piloted aircraft through a flight condition-dependent recasting of these requirements as upper bounds on the state variances. A linear matrix inequality feasibility problem is developed to compute a control law that stabilizes the system for the given flight condition while satisfying both the state variance and actuator constraints. Presented as Paper 2013-4927 at the AIAA Guidance, Navigation, and Control Conference, Boston, MA, 19-22 August 2013


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    State Variance-Based Approach to Flight Dynamic Constraints in Multidisciplinary Design Optimization




    Erscheinungsdatum :

    2017




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch



    Klassifikation :

    BKL:    55.54 Flugführung
    Lokalklassifikation TIB:    770/7040