1–12 von 12 Ergebnissen
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    Adaptive Control of Spacecraft with Flexible Appendages Using Nussbaum Gain AIAA Paper

    Lee, K. / Singh, S. | British Library Conference Proceedings | 2007

    Multi-Input Higher-Order Sliding Mode Control of Aeroelastic Systems with Uncertainties and Gust Load (AIAA 2014-0603)

    Lee, K. / Singh, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    Adaptive Output Feedback Spacecraft Formation Flying Via Observer Based Feedback Linearization

    Lee, K. / Singh, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    Internal Model Principle Based Nonlinear Robust Satellite Formation Control Despite Disturbances

    Lee, K. / Singh, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    ATTRACTIVE MANIFOLD-BASED NONCERTAINTY-EQUIVALENT ADAPTIVE CONTROL OF AIRCRAFT

    Lee, K. / Singh, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    I/O Based Variable Structure Model Reference Adaptive Satellite Formation Control in Elliptic Orbits

    Lee, K. / Singh, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    Control of a Wing Section Using Leading- and Trailing-Edge Flaps by L~1 Adaptive Feedback Despite Disturbances

    Lee, K. / Singh, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    Finite-Time Control of Satellites in Elliptic Orbits Despite Uncertainties Using Solar Radiation Pressure (AIAA 2014-0448)

    Srinivasan, L. / Lee, K. / Singh, S. et al. | British Library Conference Proceedings | 2014

    NONCERTAINTY-EQUIVALENT ADAPTIVE MISSILE CONTROL VIA IMMERSION AND INVARIANCE

    Lee, K. / Singh, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010

    AIAA-2006-6315 Global Robust Control of Aeroelastic System Using Output Feedback

    Lee, K. / Singh, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006

    Integrated Adaptive Sliding Mode Flight Control via SDU Gain Matrix Decomposition

    Lee, K. / Nambisan, P. / Singh, S. et al. | British Library Conference Proceedings | 2008

    Output Feedback Variable Structure Adaptive Control Approach to Missile Autopilot Design

    Lee, K. / Singh, S. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011