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Orbiter High Resolution Camera onboard Chandrayaan-2 Orbiter


Affiliations
1 Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
 

Orbiter High Resolution Camera (OHRC) onboard Chandrayaan-2 Orbiter-craft, is a very high spatial resolution camera operating in visible panchromatic band. OHRC’s primary goal is to image the landingsite region prior to landing for characterization and finding hazard-free zones. Post landing operation of the OHRC will be for scientific studies of small-scale features on the lunar surface. OHRC makes use of the time delay integration detector to have good signal-tonoise ratio under low illumination condition and less integration time due to very high spatial resolution. Ground sampling distance (GSD) and swath of OHRC (in nadir view) are 0.25 m and 3 km respectively, from 100 km altitude. GSD is better than 0.32 m in oblique view (25° pitch angle) during landing site imaging from 100 km altitude in two stereo views in consecutive orbits. This article includes the details of the configuration, sub-systems, imaging modes, and optical, spectral and radiometric characterization performance.

Keywords

Ground Sampling Distance, Orbiter High Resolution Camera, Relative Spectral Response, Square Wave Response, Time Delay Integration.
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  • Orbiter High Resolution Camera onboard Chandrayaan-2 Orbiter

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Authors

Arup Roy Chowdhury
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Manish Saxena
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Ankush Kumar
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
S. R. Joshi
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Amitabh
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Aditya Dagar
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Manish Mittal
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Shweta Kirkire
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Jalshri Desai
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Dhrupesh Shah
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
J. C. Karelia
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Anand Kumar
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Kailash Jha
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Prasanta Das
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
H. V. Bhagat
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Jitendra Sharma
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
D. N. Ghonia
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Meghal Desai
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Gaurav Bansal
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Ashutosh Gupta
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India

Abstract


Orbiter High Resolution Camera (OHRC) onboard Chandrayaan-2 Orbiter-craft, is a very high spatial resolution camera operating in visible panchromatic band. OHRC’s primary goal is to image the landingsite region prior to landing for characterization and finding hazard-free zones. Post landing operation of the OHRC will be for scientific studies of small-scale features on the lunar surface. OHRC makes use of the time delay integration detector to have good signal-tonoise ratio under low illumination condition and less integration time due to very high spatial resolution. Ground sampling distance (GSD) and swath of OHRC (in nadir view) are 0.25 m and 3 km respectively, from 100 km altitude. GSD is better than 0.32 m in oblique view (25° pitch angle) during landing site imaging from 100 km altitude in two stereo views in consecutive orbits. This article includes the details of the configuration, sub-systems, imaging modes, and optical, spectral and radiometric characterization performance.

Keywords


Ground Sampling Distance, Orbiter High Resolution Camera, Relative Spectral Response, Square Wave Response, Time Delay Integration.



DOI: https://doi.org/10.18520/cs%2Fv118%2Fi4%2F560-565