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研究生: 何順子
Ho, Soon-Chye
論文名稱: 微處理器控制兩軸式追蹤系統最佳化操作參數研究
Optimization of Operating Parameters for a Microprocessor-Controlled Two-axe Solar Tracker
指導教授: 鄭金祥
Cheng, Chin-Hsiang
學位類別: 碩士
Master
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2010
畢業學年度: 98
語文別: 英文
論文頁數: 62
外文關鍵詞: Microprocessor-controlled, solar tracker, operating parameter, optimization
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  • 本論文針對利用微處理器控制兩軸式追蹤系統最佳化操作參數進行分析。探討各種追蹤時間間隔及馬達耗電之操作參數對獲得最大能量及最低耗電的影響。本研究也發展出微處理器控制太陽能追蹤系統,並應用在太陽能追蹤器上進行測試。
    本研究之追蹤系統主要藉由地平座標系統追蹤太陽的運行軌道,此座標系統以追蹤器的所在地區之緯度、經度及時角計算出太陽仰角及方位角。研究中嘗試將三角函數運算已整數型態之三角函數取代,以克服(89S52)微處理器無法處理過於複雜的三角函數運算。同時,適時的線性化方位角軌跡,使得即使是在整數運算下,仍能改善太陽方位角在中午時分的誤差,提高追蹤的精確度。
    由操作參數最佳化研究發現,以四分鐘為追蹤時間間隔能在獲得最大集能比,且不消耗過多之馬達啟動耗能。實驗的結果也顯示以四分鐘為追蹤時間間隔,菲尼爾透鏡之焦點都能集中於加熱頭上,使加熱頭溫度得以維持。

    This study is concerned with the optimization of operating parameters for a microprocessor-controlled two-axe solar tracker. The operating parameters include the tracking interval and the angular rotation speed of motor. Maximum energy gain per unit energy consumption can be simulated with different tracking intervals and angular rotation speed of motors. In addiction, a microprocessor-controlled system incorporated with the solar tracker is developed.
    The microprocessor (89S52) employed in the control system is notable to deal with the complicated trigonometric function calculation. Therefore, in this study the integral trigonometric tables are built instead in the tracking program to avoid these complicated trigonometric function calculations. Meanwhile, the azimuth in the immediate period at noon is linearized by curve fitting so as to reduce the errors in the predictions of azimuth and improve the tracking accuracy.
    Results show that the maximum energy gain per unit energy consumption can be obtained when the tracking interval is 4 minutes.

    中文摘要 I Abstract II Acknowledgements III Contents IV List of Figures V Nomenclature VII Chapter 1 Introduction 1 1-1 Motivation 1 1-2 Literature survey 2 1-3 Goals of Research 3 Chapter 2 General Tracking Formulae 4 2-1 Introduction of Celestial Coordinate System 4 2-2 Ecliptical Coordinate System 4 2-3 Equatorial Coordinate System 4 2-4 Horizontal Coordinate System 5 2-5 Definition of Horizontal Coordinate System 6 2-6 Sun altitude and azimuth in Tainan 11 Chapter 3 Development of Microprocessor-Controlled Two-Axe Solar Tracker and Optimization of Operating Parameters 13 3-1 Stepping Motor Control Devices 13 3-2 Construction of Solar Tracking System 14 3-3 Control System Programming 15 3-3-1 Trigonometric Table Creating 15 3-3-2 Altitude and Azimuth Tables Creating 16 3-3-3 Time Function and GPS Receiver 16 3-3-4 Change of Altitude and Azimuth 17 3-4 Azimuth Linearizations 17 3-5 Parameters Optimization 18 3-5-1 Time Interval 18 3-5-2 Angular Speed of Stepping Motor 19 3-5-3 Energy Gain per unit Energy Consumption 20 Chapter 4 Results and Discussion 22 4-1 Case Study and Experiment Setup 22 4-2 Experiment Result 22 Chapter 5 Concluding Remarks 24 5-1 Conclusions 24 5-2 Future Studies 25 References 26 List of Figures Figure 1-1 Solar collector. (a) Traditional PV panel from STS Solar, Inc; (b) Dish solar collector and power conversion engine from Stirling Energy System, Inc (SES) 28 Figure 1-2 Comparison of irradiance, measured with Eppley phrheliometer at the tested tracker, two Eppley pyrheliometers at INTRA sun tracker and with Kipp & Zonen phyrheliometer on 13.09.2003 [1] 29 Figure 1-3 Solar radiation input in different system [5] 30 Figure 1-4 Error of incident angle from every time interval [7] 31 Figure 1-5 Efficiency of Fresnel lens versus incident angle [13] 32 Figure 2-1 Equatorial coordinate system 33 Figure 2-2 Tilt of the Earth's axis with respect to the ecliptic 34 Figure 2-3 Declination changes during a year 35 Figure 2-4 Horizontal coordinates system, Altitude, from local horizon to the target star (red), Azimuth, from the North point (green) 36 Figure 2-5 Trajectory change of Tainan (22.59N, 120.13E) at the Summer Solstice, (a) Altitude, (b) Azimuth 37 Figure 2-6 Trajectory change of Tainan (22.59N, 120.13E) at the Spring and Autumnal Equinox. (a) Altitude; (b) Azimuth 38 Figure 2-7 Trajectory change of Tainan (22.59N, 120.13E) at the Winter Solstice, (a) Altitude, (b) Azimuth 39 Figure 2-8 3-D sun trajectories during four seasons at Tainan (22.59N, 120.13E) 40 Figure 2-9 Azimuth changes (Trajectory of solar tracker) in Tainan (22.59N, 120.13E) (a) Winter Solstices (δ=-23.45˚); (b) Spring and Autumnal Equinox (δ=0˚); (c) Summer Solstices (δ=23.45˚) 41 Figure 2-10 Solar Azimuth change of a top view image in Tainan (22.59N, 120.13E), (a) Winter Solstice, (b) Spring Equinox, Autumnal Equinox, (c) Summer Solstice 42 Figure 3-1 Two-axe solar tracker designed from NCKU PEACE LAB 43 Figure 3-2 Usable Data from GPS (First column is currently time on PC, second column is UTC, third column is local latitude, and last column is local longitude) 44 Figure 3-3 Solar radiation measured in Tainan [15] 45 Figure 3-4 Solar tracking devices. (a) Microprocessor (89S52); (b) Manual Joystick; (c) GPS receiver; (d) 5-phase Stepping motor TS3630N1E1 (left), Motor driver AU9151 (right); (e) solar tracking system. 47 Figure 3-5 Flow Chart of sun tracking program 48 Figure 3-6 Trigonometric tables in control program 49 Figure 3-7 Coordinates matrix on 9 June 2010. (a) Altitude; (b) Azimuth 50 Figure 3-8 Theoretical azimuth vs. azimuth by using trigonometric. (a) Winter Solstice; (b)Spring and Autumnal Equinox; (c) Summer Solstices 51 Figure 3-9 Incident angle by using linearization. (a) Winter Solstice; (b) Spring and Autumnal Equinox; (c) Summer Solstices 52 Figure 3-10 Theoretical azimuth vs. azimuth with linearization. (a) Winter Solstice; (b) Spring and Autumnal Equinox; (c) Summer Solstices 53 Figure 3-11 Incident angle by using linearization. (a) Winter Solstice; (b) Spring and Autumnal Equinox; (c) Summer Solstices 54 Figure 3-12 Power consumption varies with different Pulse per second 56 Figure 3-13 Altitude, azimuth and incident angle different of every time interval. (a)Δτ=1 minutes; (b)Δτ =2 minutes; (c)Δτ = 3 minutes; (d)Δτ = 4 minutes. 55 Figure 3-14 Energy gain per unit energy consumption with different tracking intervals. 57 Figure 3-15 Energy consumption of stepping motor driver under taking 4 minutes as tracking interval 58 Figure 4-1 Tracking process at different moment from 13:00 to 16:00 of 9th June 59 Figure 4-2 Temperature of heating head with solar radiation on 7 June 2010 61 Figure 4-3 Temperature of heating head with solar radiation on 27 May 2010 62

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