Torque Coordinated Control of Six-Wheeled Planetary Rovers Based on Wheel–Terrain Interaction

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2025-02-17 DOI:10.1109/TAES.2025.3542746
Huaiguang Yang;Lintao Yang;Liang Ding;Chaojie Yang;Chongfu Xu;Haibo Gao;Ye Yuan;Zongquan Deng
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Abstract

Global interest in lunar exploration programs has heightened focus on the lunar South Pole region. With its complex terrain and irregular illumination, this region poses challenges for the mobility and energy management of planetary rovers. Consequently, to ensure adequate passing ability while minimizing energy consumption, research on the coordinated control of multidriven wheels is essential. In this study, a torque-coordinated control approach based on wheel–terrain interaction for a six-wheeled planetary rover is proposed. First, the continuous stress distribution model of the wheel–terrain interaction is simplified into an equivalent concentrated force model. Subsequently, precise and robust tracking of the desired velocity was achieved using a sliding-mode controller to overcome the challenges posed by model simplification and rough terrain. Subsequently, based on the expected torque obtained from the sliding-mode controller, with the optimization objective of minimizing energy consumption, the forces on the wheels were analyzed using the equivalent concentrated force model, and the torque distribution was coherently controlled. Finally, the effectiveness of the control method and the accuracy of the model are verified through whole-vehicle experiments, and the energy efficiency optimization ratio varies from 9.93% to 5.16% within the resistance range of 0–80 N.
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基于车轮-地形相互作用的六轮行星漫游车力矩协调控制
全球对月球探测计划的兴趣已经提高了对月球南极地区的关注。该地区地形复杂,光照不规则,对行星探测器的机动和能量管理提出了挑战。因此,为了在保证足够的通过能力的同时最大限度地降低能耗,对多驱动轮的协调控制进行研究是必要的。提出了一种基于车轮-地形相互作用的六轮行星漫游车力矩协调控制方法。首先,将车轮-地形相互作用的连续应力分布模型简化为等效集中力模型;随后,使用滑模控制器实现了对所需速度的精确和鲁棒跟踪,以克服模型简化和崎岖地形带来的挑战。随后,基于滑模控制器得到的期望转矩,以能量消耗最小为优化目标,采用等效集中力模型对车轮受力进行分析,并对转矩分布进行相干控制。最后,通过整车实验验证了控制方法的有效性和模型的准确性,在0 ~ 80 N阻力范围内,能效优化率为9.93% ~ 5.16%。
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来源期刊
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
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