Research on Sliding Mode and Backstepping Control of Missile Pitch Channal System
نویسندگان
چکیده
A new type of proportional plus sliding mode inversion controller is constructed and applied to solve the attack angle tracking problem missile pitch channel; At same time, in order differential explosion backstepping control, a method combining an integral surface with accurate differentiator proposed derivative desired angular rate signal; last, kind Lyapunov function prove stability boundness closed-loop signal whole system; Finally, digital simulation experiment done verify correctness method.
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ژورنال
عنوان ژورنال: Advances in computer, signals and systems
سال: 2023
ISSN: ['2371-882X', '2371-8838']
DOI: https://doi.org/10.23977/acss.2023.070501