Flight simulation system and flight simulation method for unmanned aerial vehicles
A flying vehicle and flight simulation technology, applied in the field of unmanned aerial vehicle control system, can solve problems such as difficulty for beginners, damage and crash of unmanned aerial vehicle prototypes, and achieve the effect of avoiding damage or crash.
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[0036] The present invention relates to the concepts of the unmanned aerial vehicle control system and the physical engine, so first explain the composition of the unmanned aerial vehicle control system and the function of the physical engine.
[0037] The UAV control system includes, but is not limited to the following three parts:
[0038] 1. Collective Pitch Control
[0039] The collective pitch lever for short is used to control the change of the collective pitch of the rotor blades. When the collective pitch lever is pushed up, the automatic tilter will rise as a whole to increase the total pitch of the rotor blades (that is, the pitch of all blades increases at the same angle) to increase the rotor pulling force, otherwise the pulling force will decrease, thereby controlling Helicopter (Unmanned Aerial Vehicle) lift motion.
[0040] 2. Cyclic Control: Horizontal / Vertical
[0041] Referred to as the steering column, it is connected to the automatic tilter. When operat...
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