S. M. Hoseini

Department of Electrical Engineering, Malek-e Ashtar University of Technology

[ 1 ] - 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...

[ 2 ] - طراحی و تست تجربی الگوریتم توجیه اولیه با استفاده ازخروجی سنسورهای ناوبری اینرسی

This article has no abstract.

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