Lee K. Development of unmanned aerial vehicle (UAV) for wildlife surveillance[D]. Gainesville: University of Florida, 2004.
[2]
Christiansen R S. Design of an autopilot for small unmanned aerial vehicles[D]. Provo: Brigham Young University, 2004.
[3]
Joowon P. A prototype design, test and evaluation of a small unmanned aerial vehicle for short operations, AIAA-2004-6536[R]. Reston: AIAA, 2004.
[4]
Kroo I. Design and development of the swift: a foot-launched sailplane, AIAA-2000-4336[R]. Reston: AIAA, 2000.
[5]
Wang G, Hu Y, Song B F. A flying wing UAV trimmed with propeller thrust[J]. Journal of Northwestern Polytechnical University, 2014, 32(2): 181-187 (in Chinese). 王刚, 胡峪, 宋笔锋. 利用螺旋桨动力配平的飞翼布局无人机[J]. 西北工业大学学报, 2014, 32(2): 181-187.
[6]
Dimitri N M, Oliver B, Daniel A D. Robust design simulation: a probabilistic approach to multidisciplinary design[J]. Journal of Aircraft, 1999, 36(1): 298-307.
[7]
Wang Y, Yu X Q. Optimization method for aircraft conceptual design under uncertainty[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(10): 1883-1888 (in Chinese). 王宇, 余雄庆. 考虑不确定性的飞机总体参数优化方法[J]. 航空学报, 2009, 30(10): 1883-1888.
[8]
Meng W G, Ma D L, Chu L. Wing aerodynamic robustness optimization based on neural network response surface[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(6): 1135-1140 (in Chinese). 蒙文巩, 马东立, 楚亮. 基于神经网络响应面的机翼气动稳健优化设计[J]. 航空学报, 2010, 31(6): 1135-1140.
[9]
Flachsbart O, Krober G. Experimental investigation of aircraft propellers exposed to oblique air currents, NACA TM-562[R]. Washington, D.C.: NACA, 1930.
[10]
Nickl K, Wohlfahrt M. Tailless aircraft in theory and practice[M]. Reston: AIAA Education Series, 1994: 74, 81-82, 92-93, 369-371.
[11]
Daniel S A, Nicolaas J T, Huyssen R J. Pitch handling qualities investigation of the tailless gull-wing configuration[J]. Journal of Aircraft, 2009, 46(2): 683-691.
[12]
Li J Z, Gao Z H. The application of multi-objective evolutionary algorithm and surrogate model to aerodynamic robust optimization design[J]. Acta Aerodynamic Sinica, 2012, 30(1): 47-51 (in Chinese). 李焦赞, 高正红. 多目标进化算法和代理模型技术在气动稳健优化设计中的应用[J]. 空气动力学学报, 2012, 30(1): 47-51.
[13]
Liang Y, Cheng X Q, Li Z N, et al. Multi-object aerodynamic configuration parameter design using Kriging approximation[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(6): 1141-1148 (in Chinese). 梁煜, 程小全, 郦正能, 等. 基于代理模型的气动外形平面参数多目标匹配设计[J]. 航空学报, 2010, 31(6): 1141-1148.
[14]
Garrison P, Pinella D. CMARC user's guide[M]. Los Angeles: Aerologic Inc., 2009: 21-31.
[15]
Timothy T, Brian G. Zero lift drag and drag divergence prediction for finite wings in aircraft design, AIAA-2010-0846[R]. Reston: AIAA, 2010.
[16]
Wang G, Hu Y, Song B F. Improving performance of flying wing UAV with propeller thrust involved trimming the pitching moment, AIAA-2013-4421[R]. Reston: AIAA, 2013.
[17]
Charles N A, Robert H L. Design of optimum propellers[J]. Journal of Propulsion and Power, 1994, 10(5): 676-682.
[18]
Phillips W F, Anderson E A, Kelly Q J. Predicting the contribution of running propellers to aircraft stability derivatives[J]. Journal of Aircraft, 2003, 40(6): 1107-1114.
[19]
Lawrence D A, Mohseni K. Efficiency analysis for long-endurance electric MAVs, AIAA-2005-7090[R]. Reston: AIAA, 2005.
[20]
Traub L W. Range and endurance estimates for battery-powered aircraft[J]. Journal of Aircraft, 2011, 48(2): 703-707.
[21]
Zhang K S. Multidisciplinary design optimization method and its application in aircraft design[D]. Xi'an: Northwestern Polytechnical University, 2006 (in Chinese). 张科施. 飞机设计的多学科优化方法研究[D]. 西安: 西北工业大学, 2006.