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A trim problem formulation for maximum control authority using the Attainable Moment Set geometry
CEAS Aeronautical Journal
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Aerospace Science and Technology
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A trim problem formulation for maximum control authority using the Attainable Moment Set geometry
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Aerospace Science and Technology
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A Control Allocation approach to induce the center of pressure position and shape the aircraft transient response
Aerospace Science and Technology
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AIAA Scitech 2020 Forum
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Aerospace
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A Generalized Approach to Operational, Globally Optimal Aircraft Mission Performance Evaluation, with Application to Direct Lift Control
Aerospace
journal-article
A generalized approach to operational, globally optimal aircraft mission performance evaluation, with application to direct lift control
Aerospace
journal-article
A generalized approach to operational, globally optimal aircraft mission performance evaluation, with application to direct lift control
Aerospace
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Trim for Maximum Control Authority using the Attainable Moment Set
AIAA Scitech 2020 Forum
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AIAA Aviation 2019 Forum
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AIAA AVIATION Forum, 17-21 June 2019, Dallas, Texas
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AIAA Aviation 2019 Forum
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Aerospace
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Flight Load Assessment for Light Aircraft Landing Trajectories in Windy Atmosphere and Near Wind Farms
Aerospace
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Flight Load Assessment for Light Aircraft Landing Trajectories in Windy Atmosphere and Near Wind Farms
Aerospace
journal-article
Flight load assessment for light aircraft landing trajectories in windy atmosphere and near wind farms
Aerospace
journal-article
Flight Load Assessment for Light Aircraft Landing Trajectories in Windy Atmosphere and Near Wind Farms
Aerospace
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