Design and Simulation of Double-loop Sliding Mode Controller for Missile Attitude
نویسندگان
چکیده
منابع مشابه
Adaptive Sliding Mode Controller Design For Attitude Small UAV
Received Apr 6 , 2015 Revised Aug 18 , 2015 Accepted Aug 26 , 2015 The dynamic of Unmanned Aerial Vehicle (UAV) is nonlinear, strongly coupled, multi-input multi-output (MIMO), and subject to uncertainties and external disturbances. In this paper, an adaptive sliding mode controller (ASMC) is integrated to design the attitude control system for an inner loop fixed wing UAV. In the proposed sche...
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ژورنال
عنوان ژورنال: DEStech Transactions on Computer Science and Engineering
سال: 2019
ISSN: 2475-8841
DOI: 10.12783/dtcse/cisnrc2019/33350