1–12 von 12 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 via Tube-Based Model Predictive Control

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

    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

    Development and Experimentation of a CubeSat Magnetic Attitude Control System Testbed

    Cervettini, Guglielmo / Pastorelli, Stefano / Park, Hyeongjun et al. | IEEE | 2021

    A comparative study of entry guidance for Mars robotic and human landing missions

    Lee, Youngro / Lee, Dae Young / Wie, Bong | Elsevier | 2023

    Rigid-Foldable Polyhedral Origami

    Kim, Tae-Hyun / Jang, Keon-Ik / Lee, Dae-Young et al. | AIAA | 2023