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Aircraft control often requires design compromise over various regions of flight. This work demonstrates a control strategy that takes a set of simple control laws and uses an optimization routine to combine them yielding an improved aircraft trajectory with minimal degradation to computational performance. This optimization routine can be applied to a wide variety of applications by varying the simple control laws which are used as the control strategies' building blocks.

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This page is a summary of: A Leader-Follower Control Strategy Built and Refined using Relational Maneuver Primitives for Approximating Optimal Trajectories in Real-Time, January 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2024-2760.
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