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Selecting the loop gains of the unmanned aerial vehicle pitch attitude control system with allowance for tolerances on the aerodynamic and mass centering characteristics
Authors: Fam Suan Chyong  | Published: 28.05.2018 |
Published in issue: #5(22)/2018 | |
DOI: DOI: 10.18698/2541-8009-2018-5-317 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: unmanned aerial vehicle, flight control system, attitude control system, stabilization law, cruise missile, Kharitonov theorem, D-partitioning method, robust stability |