{"title":"高通量系统中微板递送的实验室自动化无人机","authors":"Dongbin Kim, P. Oh","doi":"10.1109/ICUAS.2018.8453278","DOIUrl":null,"url":null,"abstract":"In this paper, the author presents a lab automation drone concept design for high throughput systems(HTS). A 6 degree-of-freedom (6-DOF) parallel manipulator and parallel sensorized gripper are affixed together to a rotorcraft. The manipulator-gripper allows dexterously delivery of micro-plates broadly used for sample-testing in high throughput systems. For testing and evaluation, the concept design is deployed in two pick-and-place experiments using micro-plates. First the manipulator-gripper system is attached to a gantry crane system, then it is tested on a quadcopter under manual flight within motion capture space. The results demonstrate the viability of the design and point towards future work on stability controls for autonomous flight.","PeriodicalId":246293,"journal":{"name":"2018 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"136 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":"{\"title\":\"Toward Lab Automation Drones for Micro-plate Delivery in High Throughput Systems\",\"authors\":\"Dongbin Kim, P. Oh\",\"doi\":\"10.1109/ICUAS.2018.8453278\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper, the author presents a lab automation drone concept design for high throughput systems(HTS). A 6 degree-of-freedom (6-DOF) parallel manipulator and parallel sensorized gripper are affixed together to a rotorcraft. The manipulator-gripper allows dexterously delivery of micro-plates broadly used for sample-testing in high throughput systems. For testing and evaluation, the concept design is deployed in two pick-and-place experiments using micro-plates. First the manipulator-gripper system is attached to a gantry crane system, then it is tested on a quadcopter under manual flight within motion capture space. The results demonstrate the viability of the design and point towards future work on stability controls for autonomous flight.\",\"PeriodicalId\":246293,\"journal\":{\"name\":\"2018 International Conference on Unmanned Aircraft Systems (ICUAS)\",\"volume\":\"136 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-06-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"3\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 International Conference on Unmanned Aircraft Systems (ICUAS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICUAS.2018.8453278\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 International Conference on Unmanned Aircraft Systems (ICUAS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICUAS.2018.8453278","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Toward Lab Automation Drones for Micro-plate Delivery in High Throughput Systems
In this paper, the author presents a lab automation drone concept design for high throughput systems(HTS). A 6 degree-of-freedom (6-DOF) parallel manipulator and parallel sensorized gripper are affixed together to a rotorcraft. The manipulator-gripper allows dexterously delivery of micro-plates broadly used for sample-testing in high throughput systems. For testing and evaluation, the concept design is deployed in two pick-and-place experiments using micro-plates. First the manipulator-gripper system is attached to a gantry crane system, then it is tested on a quadcopter under manual flight within motion capture space. The results demonstrate the viability of the design and point towards future work on stability controls for autonomous flight.
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