What is it about?
Spin-stabilized guided projectiles are very challenging to control. We apply for the first time a particular control technique to this class of systems and we show in simulation how it can be used to overcome this difficulty.
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This page is a summary of: Nonlinear Dynamic Inversion Flight Control Design for Guided Projectiles, Journal of Guidance Control and Dynamics, May 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g004976.
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