1–20 von 25 Ergebnissen
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    Quasi-Linear Parameter Varying Representation over Non-trim Region

    Shin, Jong-Yeob / Belcastro, Christine | AIAA | 2004

    Closed-Loop Evaluation of An Integrated Failure Identification and Fault Tolerant Control System for A Transport Aircraft

    Shin, Jong-Yeob / Belcastro, Christine / Khong, Thuan | AIAA | 2006

    Actuator Fault Diagnosis Using Two-Stage Extended Kalman Filters

    Ruschmann, Matthew / Wu, N. / Shin, Jong-Yeob | AIAA | 2010

    An LMI-based Analysis for Adaptive Flight Control with Unmodeled Input Dynamics

    Yang, Bongjun / Yucelen, Tansel / Shin, Jong-Yeob et al. | AIAA | 2010

    Design of a Pitch Axis Autopilot Control Law for an Executive Transport Aircraft

    Kaviratna, Lakmal / Chung, Gi-Yun / Shin, Jong-Yeob et al. | AIAA | 2019

    LMI-Based Analysis of An Adaptive Flight Control System with Unmatched Uncertainty

    Yang, Bong-Jun / Yucelen, Tansel / Shin, Jong-Yeob et al. | AIAA | 2010

    Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman Filter

    Caliskan, Fikret / Zhang, Youmin / Wu, N. Eva et al. | Tema Archiv | 2014

    Linear Parameter Varying Control Synthesis for Actuator Failure, Based on Estimated Parameter

    Shin, Jong-Yeob / Wu, N. Eva / Belcastro, Christine | AIAA | 2002

    LMI-Based Analysis for Stability Margins of Adaptive Flight Control

    Yang, Bong-Jun / Yucelen, Tansel / Calise, Anthony et al. | AIAA | 2009

    Blending approach of linear parameter varying control synthesis for F-16 aircraft

    Balas, Gary / Shin, Jong-Yeob / Kaya, Alpay | AIAA | 2001

    Worst case analysis of the flight control system X-38 crew return vehicle

    Shin, Jong-Yeob / Balas, Gary / Packard, Andrew | AIAA | 1999

    Pitch Control Law Analysis and Flight Test Demonstration of an Executive Transport Aircraft

    Shin, Jong-Yeob / Harden, Clay / Saeed, Nomaan et al. | AIAA | 2009