基于机翼-帆尾的高纬度跨年驻留太阳能飞机总体参数设计方法

doi:10.7527/S1000-6893.2013.0425

Abstract

Abstract:

Exploration of the capability of a solar-powered aircraft for year-round station keeping at higher latitudes is of great significance for the enhancement of its operational value. In this paper a model of power area density for PV modules arbitrarily oriented is first established which takes into consideration the temperature of the PV modules, flight altitude, flight latitude, and year-round seasons. The analysis on power absorption shows that the rotation angle of 90° is the optimal in the azimuth tracking method for a pair of sail tails in use. Secondly, a conceptual design methodology of solar-powered aircraft of a wing-sail configuration is developed which integrates the configuration design with energy absorption, and its formulations include mass component parameterization, aerodynamic efficiency, Kriging surrogate model and quantum behaved particle swarm optimization (QPSO) algorithm and its fitness function. Thirdly, a comparison of design methodology is conducted for the wing-sail configuration and wing-only configuration. Finally, a case study of the wing-sail configuration is conducted at the latitude of near 45°N and the altitude of higher than 18 km and its capabilities of operational altitude, payload-carrying and operational latitude in a whole year are investigated from 23.5°N to 55°N. The results show that in contrast with the traditional configuration, the wing-sail configuration improves power absorption characteristics at higher latitudes near winter, shortens the wingspan and reduce the wing area effectively, improves cruise velocity and makes year-round operation at higher latitudes feasible and efficient. These applications demonstrate the validity of the proposed design methodology of primary parameters of the wing-tail configuration solar-powered aircraft.

Key words: energy balance, PV module, solar-powered aircraft, tracking mode, stationary operation at higher latitudes, sail tail, primary parameter, stratosphere

CLC Number:

CHANG Min, ZHOU Zhou, WANG Rui. Primary Parameters Determination for Year-round Solar-powered Aircraft of Wing-sail Type at Higher Latitudes[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(6): 1592-1603.

References

[1] Bailey M D, Bower M V. High altitude solar power platform, NASA/TM-103578. Washington D.C.: NASA, 1992.

[2] Steven A, Fred B, Gilliam T. Design analysis methodology for solar-powered aircraft[J]. Journal of Aircraft, 1995, 32(4): 703-709.

[3] Rizzo E, Frediani A. A model for solar powered aircraft preliminary design[J]. The Aeronautical Journal, 2008, 112(1128): 57-78.

[4] Noth A. Design of solar powered airplanes for continuous flight[M]. Suisse: Ecole Polytechnique Fédérale de Lausanne at ETH ZüRICH, 2008: 37-112.

[5] Chang M, Zhou Z, Zheng Z C. Flight principles of solar-powered airplane and sensitivity analysis of its conceptual parameters[J]. Journal of Northwestern Polytechnical University, 2010, 28(5): 792-796. (in Chinese) 昌敏, 周洲, 郑志成. 太阳能飞机原理及总体参数敏度分析[J]. 西北工业大学学报, 2010, 28(5): 792-796.

[6] Shiau J K, Ma D M, Chiu C W. Optimal sizing and cruise speed determination for a solar-powered airplane[J]. Journal of Aircraft, 2010, 47(2): 622-629.

[7] Noll T E, Brown J M, Marla E, et al. Investigation of the Helios prototype aircraft mishap. Hampton VA: Langley Research Center, 2004.

[8] Chang M, Zhou Z, Cheng K, et al. Exploring the characteristics of power density of tracking PV modules for high-altitude stationary solar-powered airplanes[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(2): 273-281. (in Chinese) 昌敏, 周洲, 成柯, 等. 高空驻留太阳能飞机主动式光伏组件面功率特性研究[J]. 航空学报, 2013, 34(2): 273-281.

[9] Durisch W, Urban J, Pmestad G. Characterisation of solar cells and modules under actual operating conditions[J]. Renewable Energy, 1996, 8(1-4): 359-366.

[10] Incropera F P, Dewitt D P. Fundamentals of heat and mass transfer[M]. 7th ed. New York: John Wiley & Sons, 2011: 594-629

[11] Lophaven S N, Nielsen H B, Sndergaard J. DACE—a MATLAB Kriging toolbox, Technical Report IMM-TR-2002-12. Denmark: Technical University of Denmark, 2002.

[12] Sun M J, Zhan H. Synthesis airfoil optimization by particle swarm optimization based on global information[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(11): 2166-2173. (in Chinese) 孙美建, 詹浩. 基于全局信息的粒子群算法翼型综合优化设计[J]. 航空学报, 2010, 31(11): 2166-2173.

[13] Sun J, Feng B, Xu W B. Particle swam optimization with particles having quantum behavior//IEEE Proceeding of Congress on Evolutionary Computation, 2004.

[14] Brown S F. The eternal airplane[J]. Popular Science, 1994, 244(4): 70-75.

[15] Hall D, Fortenbach C, Dimiceli E, et al. A preliminary study of solar powered aircraft and associated power trains, NASA-CR-3699. Washington D.C.: NASA, 1983.

[16] Raymer D P. Aircraft design: a conceptual approach[M]. 3rd ed. Washington D.C.: American Institute of Aeronautics and Astronautics, Inc., 1999: 280-289.

[17] Anderson J D, Jr. Fundamentals of aerodynamics[M]. New York: McGraw-Hill International Editions, 1991: 193-226.

[18] Haws T D, Bowman W J. Thermal analysis of the pathfinder aircraft, AIAA-1999-0735. Reston: AIAA, 1999.

[19] Green M A, Emery K, Hishikawa Y, et al. Solar cell efficiency tables (Version 39)[J]. Progress in Photovoltaics: Research and Applications, 2012, 20: 12-20.

Primary Parameters Determination for Year-round Solar-powered Aircraft of Wing-sail Type at Higher Latitudes

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