Real-Time Optimal Trajectory Correction (ROTC) for Autonomous Quadrotor

N. A. Razak, R. Adnan, N. M. Thamrin, N. K. Mun, J. Johari
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Abstract

This research proposes a new algorithm known as Real-Time Optimal Trajectory Correction. The algorithm works if the quadrotor undergoes a deviation, an admissible trajectory path is generated for the quadrotor rapidly return on the straight-line route. There are two stages implicated in the algorithm. The first stage comprises a deviation scheme used to sense a deviation and formulates a vector. The second stage focuses on using the vector to generate a path via a Hermite interpolation technique integrated with time and tangent transformation schemes. A Dead Reckoning navigation technique is employed to steer the quadrotor on the path. The scheme and algorithm have experimented in low, moderate and high categories of deviation acceleration via a customized quadrotor. Comparative performance of quadrotor navigation integrated with and without the algorithm are carried out. The parameters evaluated are focused on distance and time utilized by the quadrotor to return on the route after a deviation happened. The results signify fewer distances and time are consumed by the quadrotor navigation with the algorithm to return to the route after a deviation happened as compared to its navigation without it. Conclusively, the results show the designed algorithm is relevant to assist the quadrotor autonomous navigation in a windy environment.
自主四旋翼飞行器实时最优轨迹修正(ROTC)
本研究提出了一种实时最优轨迹校正算法。该算法在四旋翼发生偏离时,生成一条允许的轨迹路径,使四旋翼在直线路线上快速返回。该算法包含两个阶段。第一阶段包括用于检测偏差的偏差方案并制定矢量。第二阶段的重点是利用向量生成路径,通过Hermite插值技术与时间和切线变换方案相结合。采用航位推算导航技术来引导四旋翼飞行器在路径上飞行。该方案和算法通过定制的四旋翼飞行器在低、中、高三类偏差加速度下进行了实验。对比了采用和不采用该算法的四旋翼飞行器导航性能。评估的参数集中在距离和时间利用四旋翼返回的路线发生偏差后。结果表明,与没有它的导航相比,四旋翼导航在偏离发生后返回路线的算法所消耗的距离和时间更少。实验结果表明,所设计的算法能够有效地辅助四旋翼飞行器在多风环境下的自主导航。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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