Taylor Reynolds

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    Comparing version 09:10, 21 Jun 2017 by treynolds with version 00:09, 19 Aug 2017 by treynolds.

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    • Control and Optimization Theory
    • Model Predictive Control & Convex Optimization approaches to spacecraft GN&C
    • Dual quaternion based 6 DoF guidance and control
    • Autonomous space operations & asteroid landing
    • Spacecraft formation flight
    • DubSat1 Project:  http://uwsatellite.com

    Publications

    • T. Reynolds and M. Mesbahi, "Small Body Precision Landing via Convex Model Predictive Control", AIAA Space Forum, Orlando, FL, 2017.
    • U. Lee, T. Reynolds, B. Barzgaran, M. Hudoba de Badyn, J. Chrisope, A. Adler, K. Kaycee and M. Mesbahi, "Development of Attitude Determination and Control Subsystem  for 3U CubeSat with Electric Propulsion", AIAA Space Forum, Orlando, FL, 2017.

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    Version from 09:10, 21 Jun 2017

    This revision modified by treynolds (Ban)

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    Version as of 00:09, 19 Aug 2017

    This revision modified by treynolds (Ban)

    ...

    • Control and Optimization Theory
    • Model Predictive Control & Convex Optimization approaches to spacecraft GN&C
    • Dual quaternion based 6 DoF guidance and control
    • Autonomous space operations & asteroid landing
    • Spacecraft formation flight
    • DubSat1 Project:  http://uwsatellite.com

    Publications

    • T. Reynolds and M. Mesbahi, "Small Body Precision Landing via Convex Model Predictive Control", AIAA Space Forum, Orlando, FL, 2017.
    • U. Lee, T. Reynolds, B. Barzgaran, M. Hudoba de Badyn, J. Chrisope, A. Adler, K. Kaycee and M. Mesbahi, "Development of Attitude Determination and Control Subsystem  for 3U CubeSat with Electric Propulsion", AIAA Space Forum, Orlando, FL, 2017.

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