EOS-08 Gnss-Reflectometry Payload Level-1 Data Product Generation

EOS-08 is an earth observing satellite, injected into 475 km Low Earth $\operatorname{Orbit}($ LEO) with 37° inclination, on $16{ }^{\text {th }}$ August 2024. GNSS Reflectometry (GNSS-R) payload on-board EOS-08 is ISRO’s first GNSS-R mission and first of its kind with dual frequency (L1 & L5) operation utilizing both Global Positioning System(GPS) and Indian Regional Navigation Satellite System(IRNSS) constellations. GNSS-R payload has two major subsystems viz. Precise Orbit Determination (POD) subsystem (comprising of two zenith antennas to receive direct GNSS signal) and Reflectometry subsystem (comprising of one nadir antenna to receive reflected signals). The direct and reflected L1 & L5 IF signals recorded onboard along with auxiliary information are send on ground for further processing. The aim of this paper is to describe generation of Level-1 data products from the sensor raw data. Data processing strategy for specular point estimation and computation of various radiometric parameters along with the product format has been discussed is this paper.

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Published
2024-12-02
DOI
https://doi.org/10.1109/ingarss61818.2024.10984412
Citations
1
Primary Topic
Calibration and Measurement Techniques
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article
Field-Weighted Citation Impact
1.30
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EOS-08 Gnss-Reflectometry Payload Level-1 Data Product Generation

Devang Mankad, V. M. Ramanujam, D. K. Jain, Parikshit Parasher et al.
1 citations
Calibration and Measurement Techniques
1.30
article

EOS-08 Gnss-Reflectometry Payload Level-1 Data Product Generation

Devang Mankad, V. M. Ramanujam, D. K. Jain, Parikshit Parasher, Puja Kakkar, Jignesh Kshatriya
article en
1 citations

Abstract

EOS-08 is an earth observing satellite, injected into 475 km Low Earth $\operatorname{Orbit}($ LEO) with 37° inclination, on $16{ }^{\text {th }}$ August 2024. GNSS Reflectometry (GNSS-R) payload on-board EOS-08 is ISRO’s first GNSS-R mission and first of its kind with dual frequency (L1 & L5) operation utilizing both Global Positioning System(GPS) and Indian Regional Navigation Satellite System(IRNSS) constellations. GNSS-R payload has two major subsystems viz. Precise Orbit Determination (POD) subsystem (comprising of two zenith antennas to receive direct GNSS signal) and Reflectometry subsystem (comprising of one nadir antenna to receive reflected signals). The direct and reflected L1 & L5 IF signals recorded onboard along with auxiliary information are send on ground for further processing. The aim of this paper is to describe generation of Level-1 data products from the sensor raw data. Data processing strategy for specular point estimation and computation of various radiometric parameters along with the product format has been discussed is this paper.

Indian Space Research Organisation (IN)
Affordable and clean energy
Openalex Percentile: Top 10%
Calibration and Measurement Techniques
1.30
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