Finite-Time Control of Wing-Rock Motion for Delta Wing Aircraft Based on Whale-Optimization Algorithm
نویسندگان
چکیده
The rise of wing-rock motion in delta-wing aircraft has an adverse effect on the manoeuvrability and it may result its crash. This study presents a finite-time control design to tackle dynamic due Wing-Rock aircraft. is developed based methodology Super Twisting Sliding Mode Control (STSMC). Lyapunov stability analysis been pursued ensure asymptotic convergence errors determine finite time. STSMC leads appearance parameters, which have direct impact performance controlled system. To avoid conventional tuning these parameters optimal proposed controller, modern optimization technique Wale Optimization Algorithm. A comparison between non-optimal super twisting sliding mode controllers established their effectiveness verified via numerical simulation using MATLAB programming format.
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ژورنال
عنوان ژورنال: Indonesian journal of science and technology
سال: 2021
ISSN: ['2527-8045', '2528-1410']
DOI: https://doi.org/10.17509/ijost.v6i3.37922