Thats a unique idea.You should consider the following idea to enhance your idea so that it would impact uniquely: An existing attitude tracking control method developed for a FlyGen airborne wind energy (AWE) system is extended to control a GroundGen AWE system. The GroundGen system produces energy through kite-generated aerodynamic forces that tension a flexible tether attached beten the kite center of gravity and a ground generator system. The kite is modelled using a six degree of freedom aircraft dynamics model.  first provide an extension of a previously developed attitude tracking theorem which shows the possibility of simultaneously tracking both the effective angle of attack and sideslip angle on the kite. A detailed aerodynamic model with empirical airfoil data and three dimensional wing tip effects is included. A feedback linearization controller is designed, and a baseline simulation is studied for confirming the tracking behavior.
['Haocheng Li', 'David J. Olinger', 'Michael A. Demetriou']
I am writing a research paper on a idea Attitude tracking control of a GroundGen airborne wind energy system
[{"from": "human", "value": "I am writing a research paper on a idea Attitude tracking control of a GroundGen airborne wind energy system"}, {"from": "gpt", "value": "Thats a unique idea.You should consider the following idea to enhance your idea so that it would impact uniquely: An existing attitude tracking control method developed for a FlyGen airborne wind energy (AWE) system is extended to control a GroundGen AWE system. The GroundGen system produces energy through kite-generated aerodynamic forces that tension a flexible tether attached beten the kite center of gravity and a ground generator system. The kite is modelled using a six degree of freedom aircraft dynamics model.  first provide an extension of a previously developed attitude tracking theorem which shows the possibility of simultaneously tracking both the effective angle of attack and sideslip angle on the kite. A detailed aerodynamic model with empirical airfoil data and three dimensional wing tip effects is included. A feedback linearization controller is designed, and a baseline simulation is studied for confirming the tracking behavior."}]