Patent Document ID: 20150039161
Application ID: 14471522
Patent Flag: 0

Claim One:
1. A control system for at least one tethered gyroglider along a flight path consistent with at least one flight mission, said control system comprising: a learning and library manager having a repository, said library manager adapted to receive and store in said repository, at least one of measured, simulated and calculated first values corresponding to at least one dynamic element associated with the at least one flight mission; at least one second value corresponding to pre-determined settings associated with the at least one flight mission; and stored flight paths associated with stored sets containing at least one of the stored first values and at least one of the stored second values, said stored flight paths corresponding to the at least one flight mission; an input manager adapted to receive current first values corresponding to the current state of said at least one dynamic element; a settings manager adapted to receive second values associated with at least one current flight mission of the at least one tethered gyroglider; a flight path controller comprising: a flight path generator adapted to receive a current set containing at least one of said current first values and at least one of said second values and the stored flight path along with the associated at least one stored set for said at least one current flight mission; said flight path generator further adapted to perform at least one of an iterative comparison, analysis, simulation, optimization, testing, ranking, rating and filtering of the received at least one current first value, with reference to the received at least one stored first value, to compute at least one corrected first value to co-operate with the received at least one second value and generate at least one determined flight path that substantially associates with said at least one current flight mission; and an editor adapted to append said stored sets with said current set containing said corrected first values, said second values and said determined flight path for said at least one current flight mission; and an activity processor adapted to receive and monitor said corrected first values and further adapted to perform at least one of allocating, segmenting, translating and transposing said corrected first values to at least one of flight control devices, generator controller, tension management means and base station control devices to achieve and generally maintain the position of the at least one tethered gyroglider along the determined flight path.