Thats a unique idea.You should consider the following idea to enhance your idea so that it would impact uniquely: The problem of autonomous take-off and landing of a tethered rigid aircraft for airborne wind energy generation is addressed. In order to accelerate the aircraft to take-off speed, the ground station is augmented with a linear motion system. An onboard propeller is used to sustain the forward velocity during the ascend of the aircraft. During landing, a slight tension on the line is kept, while the onboard control surfaces are used to align the aircraft with the rails and to land again on them. A model-based, decoupled control approach is proposed, capable to carry out a full cycle of take-off, low-tension flight, and landing again on the rails. The derived controller is tested via numerical simulations with a realistic dynamical model of the system, in presence of different wind speeds and turbulence, and its performance in terms of landing accuracy is assessed. This study is part of a project aimed to experimentally verify the take-off and landing approach on a small-scale prototype.
['Eric Nguyen Van', 'Lorenzo Fagiano', 'Stephan Schnez']
I am writing a research paper on a idea On the autonomous take-off and landing of tethered wings for airborne wind energy
[{"from": "human", "value": "I am writing a research paper on a idea On the autonomous take-off and landing of tethered wings for airborne wind energy"}, {"from": "gpt", "value": "Thats a unique idea.You should consider the following idea to enhance your idea so that it would impact uniquely: The problem of autonomous take-off and landing of a tethered rigid aircraft for airborne wind energy generation is addressed. In order to accelerate the aircraft to take-off speed, the ground station is augmented with a linear motion system. An onboard propeller is used to sustain the forward velocity during the ascend of the aircraft. During landing, a slight tension on the line is kept, while the onboard control surfaces are used to align the aircraft with the rails and to land again on them. A model-based, decoupled control approach is proposed, capable to carry out a full cycle of take-off, low-tension flight, and landing again on the rails. The derived controller is tested via numerical simulations with a realistic dynamical model of the system, in presence of different wind speeds and turbulence, and its performance in terms of landing accuracy is assessed. This study is part of a project aimed to experimentally verify the take-off and landing approach on a small-scale prototype."}]