Brigham Young University BYU ScholarsArchive All Faculty Publications 2018-11 Dynamic Optimization of High-Altitude Solar Aircraft rT ajectories Under Station-Keeping Constraints Abraham Martin Brigham Young University Nathaniel Gates Brigham Young University See next page for additional authors Follow this and additional works at: https://scholarsarchive.byu.edu/facpub Original Publication Citation Martin, R. A., Gates, N. S., Ning, A., and Hedengren, J. D., “Dynamic Optimization of High-Altitude Solar Aircraft rT ajectories Under Station-Keeping Constraints,” Journal of Guidance, Control, and Dynamics, Nov. 2018. doi:10.2514/1.G003737 BYU ScholarsArchive Citation Martin, Abraham; Gates, Nathaniel; Ning, Andrew; and Hedengren, John, "Dynamic Optimization of High-Altitude Solar Aircraft Trajectories Under Station-Keeping Constraints" (2018). All Faculty Publications. 2938. https://scholarsarchive.byu.edu/facpub/2938 This Peer-Reviewed Article is brought to you for free and open access by BYU ScholarsArchive. It has been accepted for inclusion in All Faculty Publications by an authorized administrator of BYU ScholarsArchive. For more information, please contact
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[email protected]. Authors Abraham Martin, Nathaniel Gates, Andrew Ning, and John Hedengren This peer-reviewed article is available at BYU ScholarsArchive: https://scholarsarchive.byu.edu/facpub/2938 Dynamic Optimization of High-Altitude Solar Aircraft Trajectories Under Station-Keeping Constraints R. Abraham Martin∗, Nathaniel S. Gates†, Andrew Ning‡, and John D. Hedengren§ Brigham Young University, Provo, UT, 84602 This paper demonstrates the use of nonlinear dynamic optimization to calculate energy- optimal trajectories for a high-altitude, solar-powered Unmanned Aerial Vehicle (UAV). The objective is to maximize the total energy in the system while staying within a 3 km mission radius and meeting other system constraints.