Aerodynamic framework for parachute deployment from aerial vehicle
AssigneeUnited States of America as represented by the Administrator of NASA
InventorGuru P. Guruswamy
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AssigneeUnited States of America as represented by the Administrator of NASA
InventorGuru P. Guruswamy
Estimating the term…
A computer-implemented method for determining landing conditions of an aerial vehicle includes receiving an input model representing the aerial vehicle with an internally-stored parachute and pre-determined environmental conditions, initiating a computational fluid dynamics (CFD) simulation for flight of the aerial vehicle in the pre-determined environmental conditions, receiving, from a simulation database, pre-computed aerodynamic data, including aerodynamic quantities for representing deployment of the internally-stored parachute and descent of the aerial vehicle, and coupling one or more trajectory equations with the pre-computed aerodynamic data and structural quantities of the aerial vehicle to simulate descent and landing of the aerial vehicle in the pre-determined environmental conditions via a deployed parachute.
A computer-implemented method for determining landing conditions of an aerial vehicle, the computer-implemented method comprising the steps of:
A system for generating landing condition data for an aerial vehicle, the system comprising:
A computer-implemented method for generating a simulation database of landing conditions for one or more aerial vehicles, the computer-implemented method comprising the steps of:
Dependencies are inferred from the claim text.