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An innovative high accuracy autonomous navigation method for the Mars rovers

机译:用于火星探测器的创新高精度自主导航方法

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摘要

Autonomous navigation is an important function for a Mars rover to fulfill missions successfully. It is a critical technique to overcome the limitations of ground tracking and control traditionally used. This paper proposes an innovative method based on SINS (Strapdown Inertial Navigation System) with the aid of star sensors to accurately determine the rovers position and attitude. This method consists of two parts: the initial alignment and navigation. The alignment consists of a coarse position and attitude initial alignment approach and fine initial alignment approach. The coarse one is used to determine approximate position and attitude for the rover. This is followed by fine alignment to tune the approximate solution to accurate one. Upon the completion of initial alignment, the system can be used to provide real-time navigation solutions for the rover. An autonomous navigation algorithm is proposed to estimate and compensate the accumulated errors of SINS in real time. High accuracy attitude information from star sensor is used to correct errors in SINS. Simulation results demonstrate that the proposed methods can achieve a high precision autonomous navigation for Mars rovers. © 2014 IAA.
机译:自主导航是火星探测器成功完成任务的重要功能。克服传统上地面跟踪和控制的局限性是一项关键技术。本文提出了一种基于SINS(捷联惯性导航系统)的创新方法,借助星传感器来准确确定漫游车的位置和姿态。此方法包括两部分:初始对齐和导航。对准包括粗略的位置和姿态初始对准方法和精细初始对准方法。粗略的一种用于确定流动站的大致位置和姿态。接下来是精细对齐,以将近似解调整为准确的解。初始对准完成后,该系统可用于为流动站提供实时导航解决方案。提出了一种自主导航算法来实时估计和补偿SINS的累积误差。来自恒星传感器的高精度姿态信息用于纠正SINS中的错误。仿真结果表明,所提出的方法可以实现火星漫游者的高精度自主导航。 ©2014 IAA。

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