圆形轨道重力阻尼复合纳米卫星姿态动力学研究

2023 IX International Conference on Information Technology and Nanotechnology (ITNT) Pub Date : 2023-04-17 DOI:10.1109/ITNT57377.2023.10139197

A. Doroshin, A. Eremenko

{"title":"圆形轨道重力阻尼复合纳米卫星姿态动力学研究","authors":"A. Doroshin, A. Eremenko","doi":"10.1109/ITNT57377.2023.10139197","DOIUrl":null,"url":null,"abstract":"The paper considers the attitude dynamics of a composite nanosatellite on circular orbits. The nanosatellite consists of two modules - a carrier body and a movable unit. The carrier body contains a gravitational damper. Into the movable unit a flywheel engine is installed, and the angular velocity of its rotor is constant. The mathematical model of attitude motion is built, and the numerical study of the dynamics is carried out.","PeriodicalId":296438,"journal":{"name":"2023 IX International Conference on Information Technology and Nanotechnology (ITNT)","volume":"88 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2023-04-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Investigation of the attitude dynamics of a composite nanosatellite with a gravitational damper on circular orbits\",\"authors\":\"A. Doroshin, A. Eremenko\",\"doi\":\"10.1109/ITNT57377.2023.10139197\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The paper considers the attitude dynamics of a composite nanosatellite on circular orbits. The nanosatellite consists of two modules - a carrier body and a movable unit. The carrier body contains a gravitational damper. Into the movable unit a flywheel engine is installed, and the angular velocity of its rotor is constant. The mathematical model of attitude motion is built, and the numerical study of the dynamics is carried out.\",\"PeriodicalId\":296438,\"journal\":{\"name\":\"2023 IX International Conference on Information Technology and Nanotechnology (ITNT)\",\"volume\":\"88 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2023-04-17\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2023 IX International Conference on Information Technology and Nanotechnology (ITNT)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ITNT57377.2023.10139197\",\"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 IX International Conference on Information Technology and Nanotechnology (ITNT)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ITNT57377.2023.10139197","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 0

摘要

研究了复合纳米卫星在圆轨道上的姿态动力学问题。这颗纳米卫星由两个模块组成——一个运载体和一个可移动单元。载具体内装有重力阻尼器。在活动单元内安装有飞轮发动机，其转子角速度恒定。建立了姿态运动的数学模型，并进行了动力学数值研究。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Investigation of the attitude dynamics of a composite nanosatellite with a gravitational damper on circular orbits

The paper considers the attitude dynamics of a composite nanosatellite on circular orbits. The nanosatellite consists of two modules - a carrier body and a movable unit. The carrier body contains a gravitational damper. Into the movable unit a flywheel engine is installed, and the angular velocity of its rotor is constant. The mathematical model of attitude motion is built, and the numerical study of the dynamics is carried out.

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

2023 IX International Conference on Information Technology and Nanotechnology (ITNT)

自引率

0.00%

发文量