Intelligent out-of-control protection system and method for rotary wing type unmanned aerial vehicle
A protection system and UAV technology, which is applied in the field of rotor UAV intelligent out-of-control protection system, can solve the problems that cannot meet the protection requirements of rotor UAV, the consequences are unimaginable, and difficult to control, so as to reduce the research and experiment cost, improved stability and safety, and reduced flight hazards
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Embodiment 1
[0052] Embodiment 1. An intelligent out-of-control protection system for a rotor-type UAV, including a power supply, a control chip, an attitude sensor, a height sensor, a first steering gear, a second steering gear, a catapult, a self-throwing parachute, and shock-absorbing automatic inflation Air cushion and automatic inflation device.
[0053] The power supply is used to supply power to the control chip, the attitude sensor, the height sensor, the first steering gear, the second steering gear and the catapult. Such as figure 1 A specific implementation method is given. The 6V power supply is composed of four 1.5V rechargeable batteries, which are responsible for supplying power to the entire system. In practice, any power supply that can supply power to the system can be used. In this embodiment, in order to ensure The system uses a separate power supply.
[0054] The attitude sensor and height sensor are used to obtain the attitude data and height data of the rotor UAV, ...
Embodiment 2
[0074] Embodiment 2, a kind of rotor type unmanned aerial vehicle intelligent out-of-control protection method, comprises the following steps:
[0075] The first step: establishing the intelligent out-of-control protection system of the rotor type unmanned aerial vehicle as claimed in claim 1, 2 or 3;
[0076] The second step: According to the flight motion law of the rotor UAV, through the actual flight test, obtain the threshold information of the attitude data of the rotor UAV during flight, including the threshold information of angle, angular velocity and acceleration;
[0077] Such as Figure 12 It is the determination of the out-of-control threshold of the rotor UAV angle, and then it can be obtained that when the rotor aircraft is flying normally, its pitch angle and roll angle are between -40 degrees - +40 degrees, so the out-of-control threshold angle is determined as 40 Spend.
[0078] Such as Figure 13 It is the determination of the angle out-of-control thresho...
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