i Detection of Smoke and Dust Aerosols Using Multi-sensor Satellite ...

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monochromator functions as a simple optical relay system. Located at the exit position are two reticles: one for along-scan, which is identical to the entrance slit (Fig. 7.3a), and the other for along-track (Fig. 7.3b) with stepped openings. The two reticles are positioned in turn to measure MODIS spatial response in both directions. The SRCA collimator and the MODIS optics image the reticles onto the FPAs. In the spatial mode, the IR source is on, and the lamps inside the SIS are turned on in sequence of three 10 W, two 10 W, one 10 W, and 1 W. Each band utilizes one light source configuration to assure an adequate SNR. Since the lamps need warm up time, both the along-scan and along-track measurements are performed at each lamp configuration before it is changed. Figure 7.2: The layout of the SRCA (Source: Xiong et al., 2006). 99
Figure 7.3: SRCA spatial mode reticles. (a) reticle along-scan; (b) reticle along-track (Source: Xiong et al., 2005). 7.1.3 MODIS spatial characterization using ground target approach Not all sensors, however, have an onboard calibrator like the SRCA that provides instrument on-orbit spatial calibration and characterization. Using ground measurements over specific sites for sensor on-orbit spatial characterization is one of the alternative approaches (Xie et al., 2008). For example, two targets including burning areas in the agricultural fields at the Maricopa Agricultural Center, Arizona and the Lake Pontchartrain Causeway, Louisiana are applied for spatial characterization of the NASA EO-1 advanced land imager sensor by Schowengerdt et al. (2002). Moreover, he and his coworkers selected Mackinaw Straits Bridge in Michigan and the Chesapeake Bay Bridge at Annapolis, Maryland to measure spatial characterization for HYDICE (Schowengerdt et al, 1996). The same ground target, Pontchartrain Causeway, was applied to spatial characterization by the Landsat sensor (Storey, 2001). Nelson et al. (2001) used several ground scenes including edges from glaciers as well as several 100
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Detection of Smoke and Dust Aerosol
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DEDICATION This is dedicated to my
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TABLE OF CONTENTS Page LIST OF TABL
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LIST OF TABLES Table Page Table 1.1
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Figure 6.2 The UVAI images and the
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VFM Vertical Feature Mask VIS Visib
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are validated not only visually wit
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1.1 Importance of Studying Smoke an
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1.3 Objectives and Scopes The main
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originalities, and discussions of f
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1.6 Principal Results The principle
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CHAPTER 2 REVIEW OF APPROACHES FOR
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cooperatively: the reflectance at 0
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more information about dust charact
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CHAPTER 3 SMOKE AEROSOL DETECTION W
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with a two-side scan mirror which r
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3.1.2 MODIS data The 55 0 scan angl
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Sun Satellite Figure 3.2: Basic rad
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1 0 /2 b ( 0 0, 0; , ) k1 e
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3.2.3 Training data collection Surf
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Reflectance Reflectance Response cu
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Figure 3.6: The normalized ratio of
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all pixels over both land and ocean
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NDDI 1 0.8 0.6 0.4 0.2 0 -0.2 Figur
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MODIS L1B measurements Pixels over
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is clear that most of smoke plumes
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a b c b Figure 3.10: Smoke images o
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3.4.2 California 2007 fire The 2007
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The multi-spectral approach is test
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4.1 Physical Principle of Dust Aero
Page 62 and 63: Aqua 2006 102-04/12 04:15 Terra 200
Page 64 and 65: The dust has a high reflectivity at
Page 66 and 67: 0.55 0.5 0.45 0.4 0.35 0.3 0.25 0.2
Page 68 and 69: 7 a Dust pixel 0.5 b 6 Cloud pixel
Page 70 and 71: 4.3 Results Three dust events occur
Page 72 and 73: c c Figure 4.6: Dust storm over TAK
Page 74: 4.4 Chapter Summary In this chapter
Page 77 and 78: operated in the A-train orbit with
Page 79 and 80: 5.1.2 CALIPSO measurements and VFM
Page 81 and 82: Altitude (km) 20 15 10 5 UTC: 2006-
Page 83 and 84: After spatial registration, the ove
Page 85 and 86: Figure 5.4(a) The MODIS true color
Page 87 and 88: Altitude (km) BTD (K) 20 15 10 15 4
Page 89 and 90: in the same A-train orbit with simi
Page 91 and 92: Aqua spacecrafts are operated in th
Page 93 and 94: the Fig. 6.1a. For easy comparison,
Page 95 and 96: esolutions, the number of smoke pix
Page 97 and 98: 6.1.4 Validation of dust monitoring
Page 99 and 100: Figure 6.3 Validation of dust image
Page 101 and 102: eflectance in red band. Therefore,
Page 103 and 104: Altitude (km) 20 15 10 5 UTC: 2006-
Page 105 and 106: image at the same location. The rea
Page 107 and 108: accuracy could be increased further
Page 109 and 110: FPAs and cold FPAs (because of diff
Page 111: development of future remote sensin
Page 115 and 116: 7.1.3.2 Date Source MODIS L1B data
Page 117 and 118: characterization. Only the measurem
Page 119 and 120: these bands, including reflective s
Page 121 and 122: different spectral bands are slight
Page 123 and 124: SZA (Degree) SZA (Degree) 65 60 55
Page 125 and 126: 7.2.1.2 Real Impact on L1B Measurem
Page 127 and 128: 7.2.2.1 Theoretical impact analysis
Page 129 and 130: spatial characterization, the bigge
Page 131 and 132: Difference NDDI with spatial correc
Page 133 and 134: 8.1 Conclusions CHAPTER 8 CONCLUSIO
Page 135 and 136: Based on the detection results, the
Page 137 and 138: 3) Validating aerosol detection qua
Page 139 and 140: REFERENCES Ackerman, S. A., 1989, U
Page 141 and 142: imagery, Atmospheric Environment, v
Page 143 and 144: Salomonson, V. V., Privette, J. L.,
Page 145 and 146: Martinez, A., and Gros, G., 2007-10
Page 147 and 148: Wang W., Qu, J. J., Liu, Y., Hao, X
Page 149: CURRICULUM VITAE Yong Xie is a Ph.D
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