Flight control of an airplane damaged in flight
نویسندگان
چکیده
منابع مشابه
Adaptive Quaternion Attitude Control of Aerodynamic Flight Control Vehicles
Conventional quaternion based methods have been extensively employed for spacecraft attitude control where the aerodynamic forces can be neglected. In the presence of aerodynamic forces, the flight attitude control is more complicated due to aerodynamic moments and inertia uncertainties. In this paper, a robust nero-adaptive quat...
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ژورنال
عنوان ژورنال: Proceedings of the National Aviation University
سال: 2000
ISSN: 2306-1472,1813-1166
DOI: 10.18372/2306-1472.7.11270