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    The Influence of Response Feedback Loops on the Lateral-Directional Dynamics of a Variable-Stability Transport Aircraft

    K. J. Szalai | NTIS | 1967
    Schlagwörter: Aerodynamic stability , Feedback control system , Control , Locus , Root , Stability , System

    Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings – A design perspective

    Pavel, Marilena D. / Masarati, Pierangelo / Gennaretti, Massimo et al. | Elsevier | 2015
    Schlagwörter: automatic flight control system , flight control system , linear time invariant , pilot-vehicle system , root mean square , robust stability analysis , stability augmentation system/stability and control augmentation system , thrust control lever , Flight control system design , Automatic flight control system (AFCS)