完整後設資料紀錄
DC 欄位語言
dc.contributor.authorHou, Hsin-Anen_US
dc.contributor.authorWang, Li-Chunen_US
dc.date.accessioned2019-10-05T00:09:45Z-
dc.date.available2019-10-05T00:09:45Z-
dc.date.issued2019-01-01en_US
dc.identifier.isbn978-1-7281-1217-6en_US
dc.identifier.issn1550-2252en_US
dc.identifier.urihttp://hdl.handle.net/11536/152941-
dc.description.abstractWith the inertial measurement unit (IMU) and motor technology improvement, the unmanned aerial vehicles (UAVs) become more accessible for different applications. Among the fixed-wing and the rotary-wing UAV, the former is advantageous in having no runway and small craft size which are more attractive to users. The rotary-wing UAVs is used to provide real-time monitor and control on interest targets for ground users. However, the effects of propellers are not addressed in existing rotary-wing UAV channel models. In this paper, we propose a simple air-to-ground radio communication channel for rotary-wing UAVs considering the propellers. Analysis and results are presented based on the model. The results show the maximum of Doppler shifts for all simulated frequencies exceed 300Hz, the requirement of the LTE, and there is potential risks adapt the current communication system directly for serious time-variant multipath and Doppler frequency shift channel issues.en_US
dc.language.isoen_USen_US
dc.titleAnalysis on Time-Variant Air-to-Ground Radio Communication Channel for Rotary-Wing UAVsen_US
dc.typeProceedings Paperen_US
dc.identifier.journal2019 IEEE 89TH VEHICULAR TECHNOLOGY CONFERENCE (VTC2019-SPRING)en_US
dc.citation.spage0en_US
dc.citation.epage0en_US
dc.contributor.department電信工程研究所zh_TW
dc.contributor.departmentInstitute of Communications Engineeringen_US
dc.identifier.wosnumberWOS:000482655600088en_US
dc.citation.woscount0en_US
顯示於類別:會議論文