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Trajectory Tracking for Aerial Robots: an Optimization-Based Planning and Control Approach

机译:空中机器人的轨迹跟踪:基于优化的规划和控制方法

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In this work, we present an optimization-based trajectory tracking solution for multirotor aerial robots given a geometrically feasible path. A trajectory planner generates a minimum-time kinematically and dynamically feasible trajectory that includes not only standard restrictions such as continuity and limits on the trajectory, constraints in the waypoints, and maximum distance between the planned trajectory and the given path, but also restrictions in the actuators of the aerial robot based on its dynamic model, guaranteeing that the planned trajectory is achievable. Our novel compact multi-phase trajectory definition, as a set of two different kinds of polynomials, provides a higher semantic encoding of the trajectory, which allows calculating an optimal solution but following a predefined simple profile. A Model Predictive Controller ensures that the planned trajectory is tracked by the aerial robot with the smallest deviation. Its novel formulation takes as inputs all the magnitudes of the planned trajectory (i.e. position and heading, velocity, and acceleration) to generate the control commands, demonstrating through in-lab real flights an improvement of the tracking performance when compared with a controller that only uses the planned position and heading. To support our optimization-based solution, we discuss the most commonly used representations of orientations, as well as both the difference as well as the scalar error between two rotations, in both tridimensional and bidimensional spacesSO(3) andSO(2). We demonstrate that quaternions and error-quaternions have some advantages when compared to other formulations.
机译:在这项工作中,我们给出了一个基于优化的轨迹跟踪解决方案,用于多陆航空机器人给出了几何可行路径。轨迹策划器产生最小时间,并且动态可行的轨迹,不仅包括标准限制,例如轨迹上的连续性和限制,在航路点中的约束以及计划的轨迹和给定路径之间的最大距离,还限制了基于其动态模型的空中机器人的执行器,保证计划轨迹是可实现的。我们的小型紧凑型多相轨迹定义作为一组两种不同类型的多项式,提供了轨迹的更高语义编码,轨迹允许计算最佳解决方案,而是遵循预定义的简单轮廓。模型预测控制器可确保通过具有最小偏差的空中机器人跟踪计划的轨迹。其新颖的制剂作为输入的所有规划轨迹(即位置和标题,速度和加速度)的输入,以产生控制命令,通过实验室实际航班展示与仅限的控制器相比,改善了跟踪性能的改进使用计划的位置和标题。为了支持基于优化的解决方案,我们讨论了最常用的方向表示,以及两个旋转之间的差异以及标量误差,在三维和Bidimensional Spacesso(3)和SO(2)中。我们证明与其他配方相比,四元数和误差 - 四元数有一些优势。

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