Arthur Bouton, William Reid, T. Brown, Adriana Daca, Mielad Sabzehi, H. Nayar
{"title":"行星探测漫游车备选配置与机动模式的实验研究","authors":"Arthur Bouton, William Reid, T. Brown, Adriana Daca, Mielad Sabzehi, H. Nayar","doi":"10.1109/AERO55745.2023.10115624","DOIUrl":null,"url":null,"abstract":"This paper reports on an experimental study to quantify the influence of the different adaptation capabilities that can be leveraged to improve the performance of low-cost four-wheeled rovers on sandy terrain. Conjointly with the ability to displace the center of mass and incline the rover's body, three configurations of passive suspensions and eight different locomotion modes are examined. The experiments are performed on sub-scale prototypes, with size, mass, and wheel geometry determined by a scaling analysis that ensures the consistency and transferability of the performance metrics to a 500 kg lunar rover equipped with 80 cm diameter wheels. The different configurations and locomotion modes are tested on GRC-1 lunar simulant on either a flat ground, a 20° slope or a 30° slope, while climbing uphill or downhill, with a 90° or 45° angle of attack. The performance metrics observed are the travel reduction, the lateral deviation and the energy consumption.","PeriodicalId":344285,"journal":{"name":"2023 IEEE Aerospace Conference","volume":"1071 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2023-03-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Experimental Study of Alternative Rover Configurations and Mobility Modes for Planetary Exploration\",\"authors\":\"Arthur Bouton, William Reid, T. Brown, Adriana Daca, Mielad Sabzehi, H. Nayar\",\"doi\":\"10.1109/AERO55745.2023.10115624\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper reports on an experimental study to quantify the influence of the different adaptation capabilities that can be leveraged to improve the performance of low-cost four-wheeled rovers on sandy terrain. Conjointly with the ability to displace the center of mass and incline the rover's body, three configurations of passive suspensions and eight different locomotion modes are examined. The experiments are performed on sub-scale prototypes, with size, mass, and wheel geometry determined by a scaling analysis that ensures the consistency and transferability of the performance metrics to a 500 kg lunar rover equipped with 80 cm diameter wheels. The different configurations and locomotion modes are tested on GRC-1 lunar simulant on either a flat ground, a 20° slope or a 30° slope, while climbing uphill or downhill, with a 90° or 45° angle of attack. The performance metrics observed are the travel reduction, the lateral deviation and the energy consumption.\",\"PeriodicalId\":344285,\"journal\":{\"name\":\"2023 IEEE Aerospace Conference\",\"volume\":\"1071 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2023-03-04\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2023 IEEE Aerospace Conference\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO55745.2023.10115624\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2023 IEEE Aerospace Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO55745.2023.10115624","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Experimental Study of Alternative Rover Configurations and Mobility Modes for Planetary Exploration
This paper reports on an experimental study to quantify the influence of the different adaptation capabilities that can be leveraged to improve the performance of low-cost four-wheeled rovers on sandy terrain. Conjointly with the ability to displace the center of mass and incline the rover's body, three configurations of passive suspensions and eight different locomotion modes are examined. The experiments are performed on sub-scale prototypes, with size, mass, and wheel geometry determined by a scaling analysis that ensures the consistency and transferability of the performance metrics to a 500 kg lunar rover equipped with 80 cm diameter wheels. The different configurations and locomotion modes are tested on GRC-1 lunar simulant on either a flat ground, a 20° slope or a 30° slope, while climbing uphill or downhill, with a 90° or 45° angle of attack. The performance metrics observed are the travel reduction, the lateral deviation and the energy consumption.