Formation flight method of fixed-wing unmanned aerial vehicles based on position information
A technology of formation flight and position information, applied in three-dimensional position/channel control, vehicle position/route/altitude control, instruments and other directions, can solve problems such as difficulty in applying small and low-cost unmanned aerial vehicles, and achieve the effect of low hardware requirements
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[0109] Example drone:
[0110] Without loss of generality, the formation flight method and device of the present invention are used to control the formation flight of three unmanned aerial vehicles of the same type. The overall parameters of each UAV are:
[0111] Wingspan length: 1.8m
[0112] Captain: 1.3m
[0113] Take-off weight: 4kg
[0114] Cruising flight speed: 18m / s
[0115] Minimum flying speed: 8m / s
[0116] Maximum flight speed: 28m / s
[0117] Control surfaces: aileron, elevator, rudder
[0118] Maximum roll angle limit: 35 degrees
[0119] Software and hardware design of automatic formation device:
[0120] (1) Basic composition
[0121] Both the lead plane and the wingman are equipped with the same autopilot. A typical autopilot suitable for fixed-wing UAV formation flight control is as follows: figure 2 As shown, its basic hardware includes: global positioning system (GNSS), inertial measurement unit (IMU), airspeed sensor, barometric altimeter, micro...
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