期刊資訊

Journal of Aeronautics, Astronautics and Aviation . Series A EIScopus

本刊為EI期刊

本刊為Scopus期刊

本期卷期 43:4
出刊日期 201112
刊期 季刊
ISSN 1990-7710
出版單位 中華民國航空太空學會
出刊地 台灣
出刊語言 英文
發行狀態 繼續發行/新卷期暫停授權

簡介

原刊名:中國航空太空學會學刊,發行至第37卷第4期(民94年12月)止;自民95年4月起,改為現刊名,並衍成系列A(季刊)以英文於每月三、六、九和十二月發行,系列B(半年刊)以中文(附英文摘要)於每年...

  • 本期卷期:43:4
  • 出刊日期:201112
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序號 篇名 作者 關鍵詞 下載 收藏
1 Numerical Study on the Formation of Goertler Vortices in Mixed Convection Flow over a Concave Surface with Rotation Ming-Han Lin、Chin-Tai Chen Mixed convectionGrashof numberGoertler vorticesRotationEI
2 The Effects of An On-Blade Trailing-Edge-Flap on Rotor Dynamics in Hover Yi-Ren Wang、Yin-Shing Chang HelicopterTrailing-Edge-FlapTEFInduced flowWind turbineEI
3 A Store-and-Forward Mailbox Server Design for TUUSAT-1 Communication System Roy C. Hsu、Zuu-Chang Hong、Cheng-Ting Liu、Hsien-Chu Liu Satellite communicationPACSATAutonomous ground stationTUUSATMailbox serverEI
4 Simulation of Rapid Transfer Alignment Considering Body Flexure and Data Delay on Dynamic Base Feng Qin、Xingqun Zhan、Yanhua Zhang Transfer alignmentBody flexureData delaySensor modelingInertial navigation systemKalman filterEI
5 Design and Verification of a University Microsatellite Attitude Determination and Control Subsystem Yung-Fu Tsai、Chia-Yen Chong、Jiun-Hao Huang、Ho-Nien Shou、Jiun-Jih Miau、Jyh-Ching Juang CKUTEXUniversity microsatelliteAttitude determination and controlsubsystemSoftware-in-the-loopSILprocessor-in-the-loopPILEI
6 Dynamic Structural Response Estimation of a PrintedCircuit Board Installed on a Microsatellite Due to aHalf-Sine Impact/Shock Loading Shao-Tai Lu、Syh-Tsang Jenq、Chieh Kung、Jyh-Ching Juang、Jiun-Jih Miau NCKU self-developed micro-satelliteHalf-sine shock loadingImpulsive loadingElectronic PCB structureDrop impactCKUTEXLEAPEI
7 Economic Flight Operation from Aircraft Performance Database using Correlation Analysis Chin E. Lin、Yu-Chen Liao Fuel conservationCorrelated analysisFlight Operation Quality AssuranceFOQAFlight performance databaseEI
8 The Implementation of Autonomous Formation FlightCapability to a Small Unmanned Aerial Vehicle SystemBased on Fuzzy Logic Control Yi-Ren Ding、Yi-Hsien Chen、Chia Hung Sun、Fei-Bin Hsiao Fuzzy logic controlFormation flightSmall UASEI
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