{"title":"基于Adams-Hypneu的气动无人机发射装置协同仿真方法","authors":"Chin-Fa Lee, J. Tsai, C. Kuo","doi":"10.1177/16878132231189347","DOIUrl":null,"url":null,"abstract":"The purpose of this paper is to use the co-simulation method to predict the velocity of the dummy during the launching process. Taking the PL-40 launching device of ELI Company as the research target, Adams is used to establish the mechanism model, and Hypneu establishes the pneumatic model. At the launching conditions of the 10 kg dummy and 10 bar tank pressure, the preliminary co-simulation result is compared with the launching test, and the velocity error is −3.7%. The frictional force is not a constant and depends strongly on the shuttle’s pull force during the launching process. The results are coincident with the shuttle’s kinetics equations and co-simulation results. The frictional forces between wheels and rail significantly affect the dummy’s velocity of launch devices (LDs). The effect of drag force on dummy velocity is 0.4% for the LD during launching. While the co-simulation results are compared with the reference of all conditions, and the maximum launching velocity error is −3.8%.","PeriodicalId":1,"journal":{"name":"Accounts of Chemical Research","volume":null,"pages":null},"PeriodicalIF":16.4000,"publicationDate":"2023-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Co-simulation method of pneumatic UAV launching device based on Adams-Hypneu\",\"authors\":\"Chin-Fa Lee, J. Tsai, C. Kuo\",\"doi\":\"10.1177/16878132231189347\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The purpose of this paper is to use the co-simulation method to predict the velocity of the dummy during the launching process. Taking the PL-40 launching device of ELI Company as the research target, Adams is used to establish the mechanism model, and Hypneu establishes the pneumatic model. At the launching conditions of the 10 kg dummy and 10 bar tank pressure, the preliminary co-simulation result is compared with the launching test, and the velocity error is −3.7%. The frictional force is not a constant and depends strongly on the shuttle’s pull force during the launching process. The results are coincident with the shuttle’s kinetics equations and co-simulation results. The frictional forces between wheels and rail significantly affect the dummy’s velocity of launch devices (LDs). The effect of drag force on dummy velocity is 0.4% for the LD during launching. While the co-simulation results are compared with the reference of all conditions, and the maximum launching velocity error is −3.8%.\",\"PeriodicalId\":1,\"journal\":{\"name\":\"Accounts of Chemical Research\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":16.4000,\"publicationDate\":\"2023-08-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Accounts of Chemical Research\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.1177/16878132231189347\",\"RegionNum\":1,\"RegionCategory\":\"化学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"CHEMISTRY, MULTIDISCIPLINARY\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Accounts of Chemical Research","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1177/16878132231189347","RegionNum":1,"RegionCategory":"化学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"CHEMISTRY, MULTIDISCIPLINARY","Score":null,"Total":0}
Co-simulation method of pneumatic UAV launching device based on Adams-Hypneu
The purpose of this paper is to use the co-simulation method to predict the velocity of the dummy during the launching process. Taking the PL-40 launching device of ELI Company as the research target, Adams is used to establish the mechanism model, and Hypneu establishes the pneumatic model. At the launching conditions of the 10 kg dummy and 10 bar tank pressure, the preliminary co-simulation result is compared with the launching test, and the velocity error is −3.7%. The frictional force is not a constant and depends strongly on the shuttle’s pull force during the launching process. The results are coincident with the shuttle’s kinetics equations and co-simulation results. The frictional forces between wheels and rail significantly affect the dummy’s velocity of launch devices (LDs). The effect of drag force on dummy velocity is 0.4% for the LD during launching. While the co-simulation results are compared with the reference of all conditions, and the maximum launching velocity error is −3.8%.
期刊介绍:
Accounts of Chemical Research presents short, concise and critical articles offering easy-to-read overviews of basic research and applications in all areas of chemistry and biochemistry. These short reviews focus on research from the author’s own laboratory and are designed to teach the reader about a research project. In addition, Accounts of Chemical Research publishes commentaries that give an informed opinion on a current research problem. Special Issues online are devoted to a single topic of unusual activity and significance.
Accounts of Chemical Research replaces the traditional article abstract with an article "Conspectus." These entries synopsize the research affording the reader a closer look at the content and significance of an article. Through this provision of a more detailed description of the article contents, the Conspectus enhances the article's discoverability by search engines and the exposure for the research.