| Citation: | WANG Gang, HU Yu, SONG Bi-feng, TAN Chang. Optimal design and endurance estimation of propulsion system for electric-powered unmanned aerial vehicle[J]. Journal of Aerospace Power, 2015, 30(8): 1834-1840. doi: 10.13224/j.cnki.jasp.2015.08.006
|
| [1] |
Christiansen R S.Design of an autopilot for small unmanned aerial vehicles[D].Provo:Brigham Young University,2004.
|
| [2] |
Jon N O,Bowman W J.Flight testing small,electric pow ered unmanned aerial vehicles[R].AIAA-2005-7654,2005.
|
| [3] |
Michael J L,Julio C,Mark A M.Small UAV research and evolution in long endurance electric powered vehicles[R].AIAA-2007-2730,2007.
|
| [4] |
Mustafa C,Aydan C.Optimum range and endurance of a piston propeller aircraft with cambered wing[J].Journal of Aircraft,2005,42(1):212-217.
|
| [5] |
Dale A L,Kamran M.Efficiency analysis for long-duration electric MAVs[R].AIAA-2005-7090,2005.
|
| [6] |
Ohad G,Aviv R.Optimizing electric propulsion systems for unmanned aerial vehicles[J].Journal of Aircraft,2009,46(4):1340-1353.
|
| [7] |
陈军,杨树兴,莫雳.电动无人机动力系统建模与实验[J].航空动力学报,2009,24(6):1339-1344. CHEN Jun,YANG Shuxing,MO Li.Modeling and experimental analysis of UAV electric propulsion system[J].Journal of Aerospace Power,2009,24(6):1339-1344.(in Chinese)
|
| [8] |
梁冰,王和平,袁昌盛.小型电动无人机动力系统设计和优化[J].航空计算技术,2010,40(6):78-80. LIANG Bing,WANG Heping,YUAN Changsheng.Design and optimization of power system for electric small unmanned aerial vehicle[J].Aeronautical Computing Technique,2010,40(6):78-80.(in Chinese)
|
| [9] |
刘恒,朱荣,叶雄英,等.微型飞行器航时优化[J].航空学报,2008,29(1):80-84. LIU Hen,ZHU Rong,YE Xiongying,et al.Endurance optimization for micro air vehicles[J].Acta Aeronautica et Astronautica Sinica,2008,29(1):80-94.(in Chinese)
|
| [10] |
刘斌,马晓平,王和平,等.小型电动无人机总体参数设计方法研究[J].西北工业大学学报,2005,23(3):396-400. LIU Bin,MA Xiaoping,WANG Heping,et al.Design analysis methodology for electric-powered mini-UAV[J].Journal of Northwestern Polytechnical University,2005,23(3):396-400.(in Chinese)
|
| [11] |
Retana E R,Rodrigue-Cortes H.Basic small fixed wing aircraft sizing optimizing endurance[R].Mexico City:4th Annual IEEE Conference,2007.
|
| [12] |
Lance W T.Range and endurance estimates for battery-powered aircraft[J].Journal of Aircraft,2011,48(2):703-707.
|
| [13] |
Giulio A.Maximum range for battery-powered aircraft[J].Journal of Aircraft,2013,50(1):304-307.
|
| [14] |
Blake A M,Thomas H B.Validation of vortex propeller theory for UAV design with uncertainty analysis[R].AIAA-2008-406,2008.
|
| [15] |
Charles N A,Robert H L.Design of optimum propellers[J]. Journal of Propulsion and Power,1994,10(5):676-682.
|
| [16] |
Sulivan J P,Bryan R,Phil S.Proplet propeller design/build/test final report[D].Lafayette:Purdue University,2005.
|
| [17] |
Ohad G,Aviv R.Optimization of propeller based propulsion system[J].Journal of Aircraft,2013,46(1):95-106.
|
| [18] |
Monal P M.Propeller performance measurement for low Reynolds number unmanned aerial vehicle applications[D].Wichita:Wichita State University,2004.
|
| [19] |
Michael O L,Cale Z.Analytical-experimental comparison for small electric unmanned air vehicle propellers[R].AIAA-2008-7345,2008.
|
| [20] |
Jones J L,Flynn A M.Mobile robots-inspiration to implementation[M].Wellesley:A K Peter Limited,1999.
|
| [21] |
SUN Yuhua,Jou H L,Wu J C.Multilevel Peukert equations based residual capacity estimation method for lead-acid battery[R].Piscataway:IEEE International Conference on Sustainable Energy Technologies,2008.
|
| [22] |
Dennis D,Suleiman A S.Acritical review of using the Peukert equation for determining the remaining capacity of lead-acid and lithium-ion batteries[J].Journal of Power Sources,2006,155(2):395-400.
|
| [23] |
Wagner N,Boland S,Taylor S.Powertrain design for hand-launchable long endurance unmanned aerial vehicles[R].AIAA-2011-6047,2011.
|
| [24] |
WANG Gang,HU Yu,SONG Bifeng.Improving performance of flying wing UAV with propeller thrust involved trimming the pitching moment[R].AIAA-2013-4421,2013.
|
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