High-altitude airship and high-altitude airship propulsion control method

Abstract

The present invention relates to the field of aerospace technology, and in particular to a high-altitude airship and a high-altitude airship propulsion control method. The high-altitude airship propulsion control method comprises: detecting wind field data sensed by the high-altitude airship; determining target propulsion control parameters matching the wind field data based on wind field-propulsion control parameter mapping data; the wind field-propulsion control parameter mapping data includes propulsion control parameters corresponding to different wind field data; and controlling the flight of the high-altitude airship based on the target propulsion control parameters. The high-altitude airship and the high-altitude airship propulsion control method of the embodiments of the present invention are used to solve the problem that the flight control method in the prior art has an excessively high dependence on the operator, which seriously affects the stability and safety of the long-term flight control of the high-altitude airship.

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