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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Main Authors | , , , |
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Format | Patent |
Language | Chinese English |
Published |
07.03.2023
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Subjects | |
Online Access | Get full text |
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