A new method based on motion primitives to compute 3D path planning close to helicopters' flight dynamics limits

K. Nikolajevic, N. Bélanger
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引用次数: 1

Abstract

3D path planning close to helicopters' flight dynamics limits is a critical challenge to enhance missions' assistance or autonomy. Pure dynamics model with successive integrations, Pythagorian Hodograph methods or fictive potential fields bring different drawbacks that cannot solve the problem of connecting 3D positions with associated complex set of constraints (speed orientation, curvature, torsion...) in a satisfying way. We propose in the present paper a new method based on enhanced 3D motions primitives. Their construction has been possible due to the transformation of flight loop numerical simulations into a symbolic and infinitely derivable model based on Beziers curves. Our algorithm defines strategic forms like cylinders referring to Dubins circles or vertical planes and hooks them up with the ad hoc 3D motion primitives while minimizing the curvilinear abscissa according to new principles, which are introduced. The concepts are tested for two path-planning problems and then validated against a reconstructed helicopter accident. The performance of the algorithm is measured versus an ideal Dubins-like 3D path metrics. The extremely good results we obtained pushes the challenge a step further to build up “an all flight contexts” model for the future.
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一种基于运动原语的接近直升机飞行动力学极限的三维路径规划计算方法
接近直升机飞行动力学极限的3D路径规划是提高任务辅助或自主性的关键挑战。采用连续积分的纯动力学模型、毕达哥拉斯Hodograph方法或有效势场都有不同的缺点,不能很好地解决三维位置与相关的复杂约束集(速度、方向、曲率、扭转等)的连接问题。本文提出了一种基于增强三维运动基元的新方法。由于将飞行回路数值模拟转化为基于贝塞尔曲线的符号和无限可导模型,它们的构建成为可能。我们的算法定义了策略形式,如参考杜宾圆或垂直平面的圆柱体,并将它们与特设3D运动原语挂钩,同时根据引入的新原理最小化曲线横坐标。对两个路径规划问题的概念进行了测试,然后对一个重建的直升机事故进行了验证。将算法的性能与理想的Dubins-like 3D路径指标进行比较。我们获得的非常好的结果进一步推动了未来建立“所有飞行环境”模型的挑战。
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