Fuselage return control method and system for simulating flight of unmanned aerial vehicle

The invention provides a fuselage return control method for simulating flight of an unmanned aerial vehicle. The fuselage return control method comprises the following steps: recording a simulated unmanned aerial vehicle movement input value; respectively setting the input value to a forward movemen...

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Bibliographic Details
Main Authors WANG ZHENG, GUO JIANJUN, LI SHILIN, XI QIANWEN
Format Patent
LanguageChinese
English
Published 07.03.2023
Subjects
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