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Simultaneous optimization of the vehicle design (e.g. aircraft wing size) and the trajectory (e.g. how an aircraft flies from ground to cruise altitude) can improve the performance of engineering systems. We compare numerical approaches to solve such optimization problems.
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This page is a summary of: Simultaneous Design and Trajectory Optimization Strategies for Computationally Expensive Models, AIAA Journal, February 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j063976.
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