Obstacle avoidance method and UAV under single obstacle and small obstacle in the spraying process of agricultural plant protection UAV
A technology for planting and protecting drones and drones, which is applied in aircraft parts, three-dimensional position/channel control, launching devices, etc., which can solve the problems of heavy spray and leakage, and achieve the effect of reducing the number of sprays and increasing the number of sprays.
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specific Embodiment approach 1
[0041] Specific implementation mode one: a method for avoiding obstacles under a single obstacle in the spraying process of an agricultural plant protection drone in this embodiment comprises the following steps:
[0042] Step 1) Connect the starting point and the end point of the flight path to form a straight line segment used to characterize the original flight path; this straight line segment can be used to represent a side of the spraying area, that is, in the case of no obstacles, the flight path can be It is a round-trip flight of "flying straight along one side of the spraying area → turning 180° to the next straight path". And the present invention does not consider the part of round-trip flight, only considers the situation that may run into obstacles when flying along a straight line.
[0043] Step 2) Judging whether the straight line segment intersects with the obstacle circle, if not, then fly straight along the original route, if it intersects, then perform step ...
specific Embodiment approach 2
[0053] Specific implementation mode two: the difference between this implementation mode and specific implementation mode one is:
[0054] Step 5) in, the determination method of the path length of plural optional flight paths is:
[0055] If the center of the obstacle circle and the center of the minimum turning circle are on different sides of the straight line segment, the path length of the flight path is calculated by the following formula:
[0056]
[0057] If the center of the obstacle circle and the center of the minimum turning circle are on the same side of the straight line segment, the path length of the flight path is calculated by the following formula:
[0058]
[0059] Where b is the length of the straight line segment, which is used to characterize the length of the original flight path; L is the distance from the center of the obstacle circle to the straight line segment; R is the radius of the obstacle circle; R z is the minimum turning radius of the ...
specific Embodiment approach 3
[0085] Specific embodiment 3: The difference between this embodiment and specific embodiment 1 or 2 is that the obstacle circle radius R satisfies the formula R=R d +R l , where R d is the distance from the center of the obstacle circle to the farthest edge, R l The safe distance that the UAV needs to keep from obstacles.
[0086] The geometric diagram corresponding to the above formula is as follows Image 6 shown.
[0087] The beneficial effect of this embodiment is that it takes into account the safety distance that the UAV needs to keep from obstacles due to flight jitter and external factors, which is not considered in the prior art. Further make the UAV flight path closer to the actual situation.
[0088] Other steps and parameters are the same as those in Embodiment 1 or Embodiment 2.
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