Nonlinear simulation of controller for longitudinal control augmentation system of F-16 using numerical approach

DOI10.1016/j.ins.2003.09.013zbMath1108.93036OpenAlexW1991067682MaRDI QIDQ707335

Endri Rachman, Ahmad M. Hasnah, Jihad Mohamad Jaam

Publication date: 9 February 2005

Published in: Information Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ins.2003.09.013

zbMATH Keywords

Numerical methodControl augmentation systemNonlinear simulation

Mathematics Subject Classification ID

Cites Work

• Aircraft flight controls design using output feedback

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