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

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

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NIE YING / QU ZHENGYU / ZHAO CHUNYANG / YANG YANCHU / AN GUOWEI / LI SHIQING

The invention relates to the technical field of aerospace, in particular to a high-altitude airship and a high-altitude airship propulsion control method. The high-altitude airship propulsion control method comprises the following steps: detecting wind field data sensed by the high-altitude airship; determining a target propulsion control parameter matched with the wind field data based on the wind field-propulsion control parameter mapping data; the wind field-propulsion control parameter mapping data comprises propulsion control parameters corresponding to different wind field data; and controlling the high-altitude airship to fly based on the target propulsion control parameters. The high-altitude airship and the high-altitude airship propulsion control method provided by the embodiment of the invention are used for solving the problem that the flight control method in the prior art has too high dependence on operators and seriously affects the stability and safety of long-time flight control of the high-altitude airship.

本发明涉及航空航天技术领域，尤其涉及一种高空飞艇和高空飞艇推进控制方法。高空飞艇推进控制方法，包括：检测所述高空飞艇所感知的风场数据；基于风场‑推进控制参数映射数据，确定与所述风场数据匹配的目标推进控制参数；所述风场‑推进控制参数映射数据包括不同风场数据对应的推进控制参数；基于所述目标推进控制参数控制所述高空飞艇飞行。本发明实施例的高空飞艇和高空飞艇推进控制方法，用以解决现有技术中飞行控制方法存在对操控人员的依赖性过高，严重影响高空飞艇长时飞行控制的稳定性和安全性的问题。