{"title":"利用喷气推进器控制先进载人航天器的运动","authors":"A. V. Sumarokov","doi":"10.1134/s1064230724700242","DOIUrl":null,"url":null,"abstract":"<h3 data-test=\"abstract-sub-heading\">Abstract</h3><p>The motion control of the advanced manned transport spacecraft Orel (MTSC Orel) is considered. For maneuvering and angular stabilization, a propulsion system (PS) is used as an actuator. In order to ensure simultaneous control of the motion of the center of mass of the spacecraft (SC) and its stabilization with the help of engines at each moment of time, it is necessary to solve the problems of determining the required change in the speed of the SC, choosing the optimal configuration of the engines for controlling the angular motion of the SC and correcting its orbit, and predicting the motion parameters of the SC. Methods for solving these problems, applied in the development of the control system of the manned transport spacecraft Orel, are presented. The operability of the described algorithms is confirmed by the results of mathematical modeling on a ground test bench for onboard software.</p>","PeriodicalId":50223,"journal":{"name":"Journal of Computer and Systems Sciences International","volume":null,"pages":null},"PeriodicalIF":0.5000,"publicationDate":"2024-08-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"On Controlling the Motion of an Advanced Manned Spacecraft Using Jet Thrusters\",\"authors\":\"A. V. Sumarokov\",\"doi\":\"10.1134/s1064230724700242\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<h3 data-test=\\\"abstract-sub-heading\\\">Abstract</h3><p>The motion control of the advanced manned transport spacecraft Orel (MTSC Orel) is considered. For maneuvering and angular stabilization, a propulsion system (PS) is used as an actuator. In order to ensure simultaneous control of the motion of the center of mass of the spacecraft (SC) and its stabilization with the help of engines at each moment of time, it is necessary to solve the problems of determining the required change in the speed of the SC, choosing the optimal configuration of the engines for controlling the angular motion of the SC and correcting its orbit, and predicting the motion parameters of the SC. Methods for solving these problems, applied in the development of the control system of the manned transport spacecraft Orel, are presented. The operability of the described algorithms is confirmed by the results of mathematical modeling on a ground test bench for onboard software.</p>\",\"PeriodicalId\":50223,\"journal\":{\"name\":\"Journal of Computer and Systems Sciences International\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.5000,\"publicationDate\":\"2024-08-18\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Journal of Computer and Systems Sciences International\",\"FirstCategoryId\":\"94\",\"ListUrlMain\":\"https://doi.org/10.1134/s1064230724700242\",\"RegionNum\":4,\"RegionCategory\":\"计算机科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"COMPUTER SCIENCE, ARTIFICIAL INTELLIGENCE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Computer and Systems Sciences International","FirstCategoryId":"94","ListUrlMain":"https://doi.org/10.1134/s1064230724700242","RegionNum":4,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"COMPUTER SCIENCE, ARTIFICIAL INTELLIGENCE","Score":null,"Total":0}
On Controlling the Motion of an Advanced Manned Spacecraft Using Jet Thrusters
Abstract
The motion control of the advanced manned transport spacecraft Orel (MTSC Orel) is considered. For maneuvering and angular stabilization, a propulsion system (PS) is used as an actuator. In order to ensure simultaneous control of the motion of the center of mass of the spacecraft (SC) and its stabilization with the help of engines at each moment of time, it is necessary to solve the problems of determining the required change in the speed of the SC, choosing the optimal configuration of the engines for controlling the angular motion of the SC and correcting its orbit, and predicting the motion parameters of the SC. Methods for solving these problems, applied in the development of the control system of the manned transport spacecraft Orel, are presented. The operability of the described algorithms is confirmed by the results of mathematical modeling on a ground test bench for onboard software.
期刊介绍：
Journal of Computer and System Sciences International is a journal published in collaboration with the Russian Academy of Sciences. It covers all areas of control theory and systems. The journal features papers on the theory and methods of control, as well as papers devoted to the study, design, modeling, development, and application of new control systems. The journal publishes papers that reflect contemporary research and development in the field of control. Particular attention is given to applications of computer methods and technologies to control theory and control engineering. The journal publishes proceedings of international scientific conferences in the form of collections of regular journal articles and reviews by top experts on topical problems of modern studies in control theory.
求助内容：
应助结果提醒方式：
京公网安备 11010802042870号
