共查询到18条相似文献,搜索用时 125 毫秒
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新型八轮月球车悬架的研制 总被引:9,自引:2,他引:7
提高整车质量在各轮上分配的均匀性,可提高驱动电动机驱动功率的一致性;提高悬架被动适应松软复杂地形能力,可提高其稳定性和越障能力。因此,对八轮月球车被动适应地形的悬架进行拓扑结构综合,确定两种可用的八轮悬架构型,并对这两种悬架构型进行双侧车轮同时跨越垂直障碍、适应曲面地形和车体运动平稳性仿真分析。根据分析结果,确定适合的八轮月球车悬架构型,针对这种八轮月球车移动系统的组成和工作原理进行了论述。利用ADAMS软件对悬架结构参数进行优选,在此基础上进行悬架和差动装置的结构设计,并加工出原理样机。对原理样机进行爬坡、越障等性能试验,试验结果表明:各轮载荷分布较均匀,适应地形能力强,能够爬上坡度为22°的松软沙地,越过200 mm高的障碍。 相似文献
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高通过性与平稳性月球车移动系统设计 总被引:3,自引:1,他引:2
月表行驶环境恶劣,这对月球车移动系统提出了更高的要求。为提高月球车的移动能力,提出一种具有高通过性和载荷平台平稳性的新型月球车移动系统。该移动系统由正反四边形机构悬架和伸缩叶片复式步行轮组成。正反四边形悬架是一种适用于六轮月球车的非独立悬架,通过与摇臂式悬架进行受力和姿态运动的对比分析和仿真对比分析可知,它可以使月球车具有较高的越障性能并在越障过程中保证载荷平台的相对平稳。同时,针对不同松散程度的月壤,根据车轮―土壤力学原理,设计出伸缩叶片复式步行轮。该种车轮最突出的特点是能够根据车轮与土壤间的相互作用关系,自适应调节叶片入土深度,从而改变车轮的牵引能力、平顺性和能耗。对该种移动系统进行多项移动性能试验,结果表明,该种新型移动系统具有较高的越障能力和保持载荷平台平稳能力,能够在恶劣路况下最大限度的发挥车轮的牵引能力,而且在路面通过性良好时尽可能的节约能耗,增加车轮滚动的平顺性。 相似文献
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行星轮式月球车移动系统的关键技术 总被引:6,自引:0,他引:6
为提高月球车的越障能力,重点考虑提高车轮的越障能力,成功研制了一种采用扭杆弹簧和磁弹簧减振器并联悬架,且每个行星车轮独立驱动的月球车。在行星车轮不翻转越障条件下,推导了月球车两个前行星车轮同时越障时可以爬过的垂直障碍高度与车辆参数的关系,并进行了ADAMS仿真。对行星轮式月球车进行了动力学分析,确定了行星车轮的等效地面不平度函数,并在此基础上建立了7自由度月球车振动系统模型,根据模型的计算结果确定了扭杆弹簧刚度和减振器阻尼的最佳参数范围。同时,进行了月球车爬坡试验和垂直越障能力试验研究,还模拟月球的低重力环境进行了整车的低重力试验。 相似文献
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The prober with an immovable lander and a movable rover is commonly used to explore the Moon’s surface. The rover can complete the detection on relatively flat terrain of the lunar surface well, but its detection efficiency on deep craters and mountains is relatively low due to the difficulties of reaching such places. A lightweight four-legged landing and walking robot called “FLLWR” is designed in this study. It can take off and land repeatedly between any two sites wherever on deep craters, mountains or other challenging landforms that are difficult to reach by direct ground movement. The robot integrates the functions of a lander and a rover, including folding, deploying, repetitive landing, and walking. A landing control method via compliance control is proposed to solve the critical problem of impact energy dissipation to realize buffer landing. Repetitive landing experiments on a five-degree-of-freedom lunar gravity testing platform are performed. Under the landing conditions with a vertical velocity of 2.1 m/s and a loading weight of 140 kg, the torque safety margin is 10.3% and 16.7%, and the height safety margin is 36.4% and 50.1% for the cases with or without an additional horizontal disturbance velocity of 0.4 m/s, respectively. The study provides a novel insight into the next-generation lunar exploration equipment. 相似文献
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Virtual simulation system with path-following control for lunar rovers moving on rough terrain 总被引:1,自引:0,他引:1
Virtual simulation technology is of great importance for the teleoperation of lunar rovers during the exploration phase,as well as the design of locomotion systems,performance evaluation,and control strategy verification during the R&D phase.The currently used simulation methods for lunar rovers have several disadvantages such as poor fidelity for wheel-soil interaction mechanics,difficulty in simulating rough terrains,and high complexity making it difficult to realize mobility control in simulation systems.This paper presents an approach for the construction of a virtual simulation system that integrates the features of 3D modeling,wheel-soil interaction mechanics,dynamics analysis,mobility control,and visualization for lunar rovers.Wheel-soil interaction experiments are carried out to test the forces and moments acted on a lunar rover’s wheel by the soil with a vertical load of 80 N and slip ratios of 0,0.03,0.05,0.1,0.2,0.3,0.4,and 0.6.The experimental results are referenced in order to set the parameters’ values for the PAC2002 tire model of the ADAMS/Tire module.In addition,the rough lunar terrain is simulated with 3DS Max software after analyzing its characteristics,and a data-transfer program is developed with Matlab to simulate the 3D reappearance of a lunar environment in ADAMS.The 3D model of a lunar rover is developed by using Pro/E software and is then imported into ADAMS.Finally,a virtual simulation system for lunar rovers is developed.A path-following control strategy based on slip compensation for a six-wheeled lunar rover prototype is researched.The controller is implemented by using Matlab/Simulink to carry out joint simulations with ADAMS.The designed virtual lunar rover could follow the planned path on a rough terrain.This paper can also provide a reference scheme for virtual simulation and performance analysis of rovers moving on rough lunar terrains. 相似文献
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SHANG Jianzhong School of Mechanical Science Engineering Huazhong University of Science Technology Wuhan China LUO Zirong LI Shengyi School of Mechatronics Engineering Automation National University of Defense Technology Changsha China TANG Li School of Mechanical Science Engineering Huazhong University of Science Technology Wuhan China 《机械工程学报(英文版)》2006,19(2):187-190
The mission and function requirements of lunar rover are analyzed, based on virtual prototype technology, the mobility evaluation theory and method for wheeled space rover are proposed, which provide a new way to study the innovative design of lunar rover. Based on the above theoretical system, an innovative lunar rover suspension system, which adopts a two-crank-slider mechanism, is proposed, and its dynamics model is created. Adopting virtual prototype technology, the ground adaptability, over-obstacle ability and driving placidity of the rover are evaluated in the virtual prototype software ADAMS. The analysis results show that the rover provides a high degree of mobility. 相似文献
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