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We evaluate different architectures for the pitch rate, angle of attack, and load factor control laws and implement an integrated architecture where some of the feedback paths are shared by the control laws, resulting in fewer gains to adjust, gains harmonization, and simpler mode transitions.

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This page is a summary of: Longitudinal Flight Control Law Design with Integrated Envelope Protection, Journal of Guidance Control and Dynamics, September 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g006443.
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