Aircraft Pitch Control via Second-Order Sliding Technique
نویسندگان
چکیده
منابع مشابه
Aircraft Pitch Control Via Second Order Sliding Technique
Control of high-performance low-cost unmanned air vehicles involves the problems of incomplete measurements, external disturbances and modeling uncertainties. Sliding mode control combines high precision with robustness to the aforementioned factors. The idea behind this approach is the choice of a particular constraint which, when maintained, will provide the process with the required features...
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ژورنال
عنوان ژورنال: Journal of Guidance, Control, and Dynamics
سال: 2000
ISSN: 0731-5090,1533-3884
DOI: 10.2514/2.4591