Geometric correction of synchronous scanned Operational Modular Imaging Spectrometer II hyperspectral remote sensing images using spatial positioning data of an inertial navigation system
被引:15
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作者:
Zhou, Xiaohu
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Northwest Univ, Dept Geol, Xian 710069, Shaanxi, Peoples R China
Northwest Univ, State Key Lab Continental Dynam, Xian 710069, Shaanxi, Peoples R China
Salzburg Univ, Dept Geog & Geol, A-5020 Salzburg, AustriaNorthwest Univ, Dept Geol, Xian 710069, Shaanxi, Peoples R China
Zhou, Xiaohu
[1
,2
,3
]
Neubauer, Franz
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Salzburg Univ, Dept Geog & Geol, A-5020 Salzburg, AustriaNorthwest Univ, Dept Geol, Xian 710069, Shaanxi, Peoples R China
Neubauer, Franz
[3
]
Zhao, Dong
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机构:
Northwest Univ, Dept Geol, Xian 710069, Shaanxi, Peoples R China
Northwest Univ, State Key Lab Continental Dynam, Xian 710069, Shaanxi, Peoples R ChinaNorthwest Univ, Dept Geol, Xian 710069, Shaanxi, Peoples R China
Zhao, Dong
[1
,2
]
Xu, Shichao
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h-index: 0
机构:
Northwest Univ, Dept Geol, Xian 710069, Shaanxi, Peoples R China
Northwest Univ, State Key Lab Continental Dynam, Xian 710069, Shaanxi, Peoples R ChinaNorthwest Univ, Dept Geol, Xian 710069, Shaanxi, Peoples R China
Xu, Shichao
[1
,2
]
机构:
[1] Northwest Univ, Dept Geol, Xian 710069, Shaanxi, Peoples R China
[2] Northwest Univ, State Key Lab Continental Dynam, Xian 710069, Shaanxi, Peoples R China
[3] Salzburg Univ, Dept Geog & Geol, A-5020 Salzburg, Austria
The high-precision geometric correction of airborne hyperspectral remote sensing image processing was a hard nut to crack, and conventional methods of remote sensing image processing by selecting ground control points to correct the images are not suitable in the correction process of airborne hyperspectral image. The optical scanning system of an inertial measurement unit combined with differential global positioning system (IMU/DGPS) is introduced to correct the synchronous scanned Operational Modular Imaging Spectrometer II (OMIS II) hyperspectral remote sensing images. Posture parameters, which were synchronized with the OMIS II, were first obtained from the IMU/DGPS. Second, coordinate conversion and flight attitude parameters' calculations were conducted. Third, according to the imaging principle of OMIS II, mathematical correction was applied and the corrected image pixels were resampled. Then, better image processing results were achieved. (C) 2015 Society of Photo-Optical Instrumentation Engineers (SPIE).