首页 | 本学科首页   官方微博 | 高级检索  
     检索      

滑转条件下月球车轮沉陷模型研究
引用本文:金大玮,李建桥,党兆龙,陈百超,邹猛.滑转条件下月球车轮沉陷模型研究[J].航空学报,2013,34(5):1215-1221.
作者姓名:金大玮  李建桥  党兆龙  陈百超  邹猛
作者单位:1. 吉林大学仿生工程教育部重点实验室,吉林长春 130025;空军航空大学飞行器与动力系,吉林长春 130022
2. 吉林大学仿生工程教育部重点实验室,吉林长春,130025
3. 中国空间技术研究院,北京,100094
基金项目:国家自然科学基金,国家"863"计划
摘    要: 月球车在月面行驶时,为保证月球车的通过性能,应尽量避免沉陷。然而传统车辆沉陷量数学模型不适用于动态滑转条件下的月球车,为此对月球车行驶时车轮沉陷量的计算模型进行了研究。基于车辆地面力学理论,从模拟月壤力学参数和滑转率两个方面,在适合于刚性轮静态沉陷计算模型基础上建立了适用于滑转条件下月球车轮的沉陷计算模型。通过轮壤土槽试验,将试验测得的月球车轮沉陷量与模型计算得到的沉陷量进行比较,验证了修正模型的正确性。所研究的模型能够为滑转条件下月球车沉陷量的预测提供理论技术基础。

关 键 词:月球车轮  月球着陆  滑转  模拟月壤  沉陷量  计算模型  

Study on Model for Sinkage of Lunar Rover Wheel Under Slip
JIN Dawei , LI Jianqiao , DANG Zhaolong , CHEN Baichao , ZOU Meng.Study on Model for Sinkage of Lunar Rover Wheel Under Slip[J].Acta Aeronautica et Astronautica Sinica,2013,34(5):1215-1221.
Authors:JIN Dawei  LI Jianqiao  DANG Zhaolong  CHEN Baichao  ZOU Meng
Institution:1. Key Laboratory of Bionic Engineering (Ministry of Education), Jilin University, Changchun 130025, China;
2. Aircraft and Dynamics Department, Aviation University of the Air Force, Changchun 130022, China;
3. China Academy of Space Technology, Beijing 100094, China
Abstract:In order to ensure its passing ability, a lunar rover should avoid sinkage when it is running on the lunar surface. However, the conventional calculation model of sinkage is not suitable for the lunar rover in the state of dynamic slip. Therefore, a calculation model for the sinkage of wheels is analyzed in this paper. Using the theory of terrain-mechanics, the calculation model for singkage under slip is established based on a calculation model for static sinkage from the two aspects of mechanical parameters and slip ratios. The sinkages obtained by the soil-bin test are compared with those calculated by the model and the calculation model is thus verified. The calculation model may provide the theoretical basis for the prediction of lunar rover sinkage.
Keywords:lunar rover wheel  lunar landing  slip  lunar soil simulant  sinkage  calculation model
本文献已被 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号