Quaternion Error-Based Optimal Control Applied to Pinpoint Landing
نویسنده
چکیده
Surrey Space Centre Department of Electrical and Electronic Engineering Faculty of Engineering and Physical Sciences Doctor of Philosophy
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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