1–10 von 14 Ergebnissen
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    Large-Scale Multidisciplinary Optimization of a Small Satellite’s Design and Operation

    Hwang, John T. / Lee, Dae Young / Cutler, James W. et al. | AIAA | 2014

    Maximizing photovoltaic power generation of a space-dart configured satellite

    Lee, Dae Young / Cutler, James W. / Mancewicz, Joe et al. | Elsevier | 2015

    Geometric Mechanics Based Nonlinear Model Predictive Spacecraft Attitude Control with Reaction Wheels

    Lee, Dae Young / Gupta, Rohit / Kalabić, Uroš V. et al. | AIAA | 2016

    Attitude Control of a Small Spacecraft for Earth Observation via Tube-based Robust Model Predictive Control

    Mammarella, Martina / Lee, Dae Young / Park, Hyeongjun et al. | AIAA | 2018

    ATTITUDE CONTROL OF A SMALL SPACECRAFT FOR EARTH OBSERVATION VIA TUBE-BASED ROBUST MODEL PREDICTIVE CONTROL (AIAA 2018-5401)

    Mammarella, Martina / Lee, Dae Young / Park, Hyeongjun et al. | British Library Conference Proceedings | 2018

    Attitude Control of a Small Spacecraft via Tube-Based Model Predictive Control

    Mammarella, Martina / Lee, Dae Young / Park, Hyeongjun et al. | AIAA | 2019

    DESIGN OPTIMIZATION OF A SPACE VIRTUAL TELESCOPE MISSION USING A CUBSEAT SWARM

    Park, Hyeongjun / Lee, Dae Young / Stochaj, Steven et al. | TIBKAT | 2020

    A Case Study in Formal Specification and Runtime Verification of a CubeSat Communications System

    Luppen, Zachary A. / Lee, Dae Young / Rozier, Kristin Y. | AIAA | 2021

      A CASE STUDY IN FORMAL SPECIFICATION AND RUNTIME VERIFICATION OF A CUBESAT COMMUNICATIONS SYSTEM

      Luppen, Zachary A. / Lee, Dae Young / Rozier, Kristin Y. | TIBKAT | 2021