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Acceleration based manoeuvre flight control system for unmanned aerial vehicles
(Stellenbosch : Stellenbosch University, 2008-12)
A strategy for the design of an effective, practically feasible, robust, computationally efficient autopilot for three dimensional manoeuvre flight control of Unmanned Aerial Vehicles is presented. The core feature of ...
Hover control for a vertical take-off and landing vehicle
(Stellenbosch : University of Stellenbosch, 2009-03)
This thesis details the development and comparison of two linear control systems that performhover control for a vertical take-off and landing unmanned aerial vehicle. A non-linear mathematical model of the aircraft ...