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Path planner based on bidirectional spline-RRT¿¿¿ for fixed-wing UAVs

机译:基于双向样条RRT的路径规划器,用于固定翼无人机

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This paper proposes a bidirectional spline-RRT¿¿¿ path planning algorithm for fixed-wing unmanned aerial vehicles (UAVs). The proposed algorithm combines the basic RRT¿¿¿ algorithm with the spline method to produce smooth paths, which are essential for fixed-wing UAVs. The proposed bidirectional spline-RRT¿¿¿ algorithm generates paths satisfying approach direction constraints on both start and goal points, which makes it significantly different from typical path planning algorithms. Further, the algorithm is asymptotically optimal as the cost of the path found decreases as the number of vertices increases, with the path found finally converging to the optimal path. The proposed algorithm also considers the aerodynamic characteristics of the target aircraft. As a result, the paths produced are within load factor and thrust-to-weight ratio limits, are geometrically and dynamically feasible, sub-optimal, and satisfy approach direction constraints. The results of several simulations conducted confirm these properties of the bidirectional spline-RRT¿¿¿ algorithm. In particular, the results of a nonlinear six degree-of-freedom simulation verify the aerodynamic characteristics for the target aircraft, and show that the proposed bidirectional spline-RRT¿¿¿ algorithm can be effectively utilized in path planning problems for fixed-wing UAVs.
机译:本文提出了一种用于固定翼无人机的双向样条RRT路径规划算法。所提出的算法结合了基本的RRT算法和样条方法来产生平滑的路径,这对于固定翼无人机至关重要。所提出的双向样条RRT算法可以在起始点和目标点上生成满足进近方向约束的路径,这使其与典型的路径规划算法显着不同。此外,该算法是渐近最优的,因为找到的路径的成本随着顶点数量的增加而减少,最终找到的路径收敛到最优路径。所提出的算法还考虑了目标飞机的空气动力学特性。结果,所产生的路径在负载因子和推力重量比极限之内,在几何和动态上可行,次优,并且满足进近方向约束。进行的几次仿真的结果证实了双向样条RRT算法的这些特性。特别地,非线性六自由度仿真的结果验证了目标飞机的空气动力学特性,并表明所提出的双向样条-RRT算法可以有效地用于固定翼无人机的路径规划问题中。 。

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