Method for determining optimal path of flight vehicle based on self-adaptive A star algorithm
A technology of optimal path and determination method, which is applied in the direction of navigation calculation tools, etc., can solve the problems of inability to adapt to dynamics, reduce the degree of dependence, and fail to calculate the overall path, so as to overcome the lack of robustness, shorten the length of the path, and reduce the number of waypoints. Reduced effect
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[0033] The steps of the present invention will be further described in detail below in conjunction with the accompanying drawings.
[0034] refer to figure 1 , the implementation steps of the present invention are as follows:
[0035] Step 1. Set the start point and end point of the aircraft, that is, mark the start point SP and end point EP of the aircraft on the map.
[0036] Step 2. Generate obstacle areas.
[0037] 2a) Establish a Cartesian coordinate system according to the positions of the starting point SP and the ending point EP of the aircraft;
[0038] 2b) Let p i ,q i Respectively, the coordinates of the starting point and the ending point of each obstacle that the aircraft needs to bypass, for p i Points are respectively made a straight line perpendicular to the X-axis and Y-axis of the Cartesian coordinate system, for q iThe points are respectively drawn as straight lines perpendicular to the X-axis and Y-axis of the Cartesian coordinate system, and a rectan...
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