{"title":"面向多颗低轨卫星通信的大规模MIMO上行传输","authors":"Ziyu Xiang;Rui Sun;Xinrui Gong;Xiqi Gao;Ke-Xin Li;Wenjing Liu;Xiang-Gen Xia","doi":"10.1109/TAES.2024.3508672","DOIUrl":null,"url":null,"abstract":"In this article, we investigate massive multiple-input–multiple-output (MIMO) uplink (UL) transmission for multiple low-Earth-orbit satellite communication. The signal and channel models are established for the UL massive MIMO multisatellite system. We reveal that the signals transmitted from the user terminals (UTs), which are intended for different satellites, are typically asynchronous at each satellite. We propose linear precoding with frequency and time precompensations at each UT for each satellite so that the signals intended for a specific satellite from different UTs can be synchronized. We formulate the ergodic sum rate maximization problem by considering the minimum mean square error successive interference cancellation receiver at each satellite with perfect instantaneous channel state information (iCSI). We propose a Riemannian conjugate gradient (RCG)-based precoding vector design algorithm within the manifold optimization framework, which does not include any matrix inversion. Then, in order to reduce the complexity in implementation at satellites, we reformulate the UL ergodic sum rate maximization problem by considering the linear receiving at each satellite with statistical CSI (sCSI) only. We devise an RCG-based joint precoding and receiving vector design to maximize the sum rate, which avoids any matrix inversion, thereby reducing the computational complexity. Simulation results indicate the effectiveness of our proposed approaches.","PeriodicalId":13157,"journal":{"name":"IEEE Transactions on Aerospace and Electronic Systems","volume":"61 2","pages":"4852-4865"},"PeriodicalIF":5.7000,"publicationDate":"2024-11-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Massive MIMO Uplink Transmission for Multiple LEO Satellite Communication\",\"authors\":\"Ziyu Xiang;Rui Sun;Xinrui Gong;Xiqi Gao;Ke-Xin Li;Wenjing Liu;Xiang-Gen Xia\",\"doi\":\"10.1109/TAES.2024.3508672\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this article, we investigate massive multiple-input–multiple-output (MIMO) uplink (UL) transmission for multiple low-Earth-orbit satellite communication. The signal and channel models are established for the UL massive MIMO multisatellite system. We reveal that the signals transmitted from the user terminals (UTs), which are intended for different satellites, are typically asynchronous at each satellite. We propose linear precoding with frequency and time precompensations at each UT for each satellite so that the signals intended for a specific satellite from different UTs can be synchronized. We formulate the ergodic sum rate maximization problem by considering the minimum mean square error successive interference cancellation receiver at each satellite with perfect instantaneous channel state information (iCSI). We propose a Riemannian conjugate gradient (RCG)-based precoding vector design algorithm within the manifold optimization framework, which does not include any matrix inversion. Then, in order to reduce the complexity in implementation at satellites, we reformulate the UL ergodic sum rate maximization problem by considering the linear receiving at each satellite with statistical CSI (sCSI) only. We devise an RCG-based joint precoding and receiving vector design to maximize the sum rate, which avoids any matrix inversion, thereby reducing the computational complexity. Simulation results indicate the effectiveness of our proposed approaches.\",\"PeriodicalId\":13157,\"journal\":{\"name\":\"IEEE Transactions on Aerospace and Electronic Systems\",\"volume\":\"61 2\",\"pages\":\"4852-4865\"},\"PeriodicalIF\":5.7000,\"publicationDate\":\"2024-11-28\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE Transactions on Aerospace and Electronic Systems\",\"FirstCategoryId\":\"94\",\"ListUrlMain\":\"https://ieeexplore.ieee.org/document/10770862/\",\"RegionNum\":2,\"RegionCategory\":\"计算机科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Aerospace and Electronic Systems","FirstCategoryId":"94","ListUrlMain":"https://ieeexplore.ieee.org/document/10770862/","RegionNum":2,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
Massive MIMO Uplink Transmission for Multiple LEO Satellite Communication
In this article, we investigate massive multiple-input–multiple-output (MIMO) uplink (UL) transmission for multiple low-Earth-orbit satellite communication. The signal and channel models are established for the UL massive MIMO multisatellite system. We reveal that the signals transmitted from the user terminals (UTs), which are intended for different satellites, are typically asynchronous at each satellite. We propose linear precoding with frequency and time precompensations at each UT for each satellite so that the signals intended for a specific satellite from different UTs can be synchronized. We formulate the ergodic sum rate maximization problem by considering the minimum mean square error successive interference cancellation receiver at each satellite with perfect instantaneous channel state information (iCSI). We propose a Riemannian conjugate gradient (RCG)-based precoding vector design algorithm within the manifold optimization framework, which does not include any matrix inversion. Then, in order to reduce the complexity in implementation at satellites, we reformulate the UL ergodic sum rate maximization problem by considering the linear receiving at each satellite with statistical CSI (sCSI) only. We devise an RCG-based joint precoding and receiving vector design to maximize the sum rate, which avoids any matrix inversion, thereby reducing the computational complexity. Simulation results indicate the effectiveness of our proposed approaches.
期刊介绍:
IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.