Semmling, Maximilian and Moreno Bulla, Mario Andres and Zus, Florian and Stienne, Georges and Hoque, Mohammed Mainul and Wickert, Jens and Nahavandchi, Hossein and Dielacher, Andreas and Voigtmann, Thomas and Berdermann, Jens (2024) Ionospheric delay in GNSS reflectometry: studying satellite and sounding rocket scenarios. IAG Workshop: GNSS Reflectometry 2024, 2024-11-26 - 2024-11-27, Potsdam, Germany.
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Abstract
The ionosphere induced delay in GNSS reflectometry (GNSS-R) observations is a promising research topic. Early concepts for space-borne application of GNSS-R in the 1990's pointed out already that precise altimetric monitoring over the global oceans and sea-ice areas can profit from additional GNSS-R data to mitigate ionospheric bias. Studying the ionospheric impact in GNSS-R can be challenging due to the different locations where the signal path crosses the ionospheric layers. The study has to consider the incident, reflected and the direct ray that connect transmitter, specular point and receiver. The height of the receiver platform plays an important role as the relevant refractive delays originate often from the atmosphere below. Satellite-based observations, with receiver heights usually above 350 km, experience a significantly higher ionospheric delay compared to airborne observations that at most can reach receiver heights of 20 km. In this study we investigate ionospheric delays in GNSS-R for receiver heights in the range between 10 km and 600 km, it means from common aircraft flight levels to typical low Earth orbits. This range is most important for ionospheric research as it starts below the relevant ionospheric layers (E, F) and ends considerably above typical F-layer peak heights (250-350 km). The major objective of this study is to clarify how changes in the height of ionospheric layers will affect delay and Doppler observations in GNSS-R for different receiver heights. Simulations are conducted for receivers in two GNSS-R scenarios: (1) on the PRETTY satellite (orbit height: ~550 km) and (2) on a MAPHEUS sounding rocket (with heights: 10 to 240 km). The simulation results show that for PRETTY orbit heights the budget of ionospheric delays is especially sensitive to the F-layer location (more precisely to its penetration by the direct ray). This F-layer sensitivity occurs in grazing angle geometry. It will be further quantified in the on-going study. These simulation results will help to evaluate whether GNSS-R data from a satellite like PRETTY (acquiring data in orbit since Feb. 2024) or from a sounding rocket like MAPHEUS (launch planned for Nov. 2024) can be used to monitor the variability of ionospheric layers.
| Item URL in elib: | https://elib.dlr.de/209660/ | ||||||||||||||||||||||||||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||||||||||||||||||||||||||||||
| Title: | Ionospheric delay in GNSS reflectometry: studying satellite and sounding rocket scenarios | ||||||||||||||||||||||||||||||||||||||||||||
| Authors: |
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| Date: | November 2024 | ||||||||||||||||||||||||||||||||||||||||||||
| Refereed publication: | No | ||||||||||||||||||||||||||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||||||||||||||||||||||
| In SCOPUS: | No | ||||||||||||||||||||||||||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||||||||||||||||||||||
| Keywords: | Ionospheric delay, GNSS refletometry, MAPHEUS program, PRETTY mission | ||||||||||||||||||||||||||||||||||||||||||||
| Event Title: | IAG Workshop: GNSS Reflectometry 2024 | ||||||||||||||||||||||||||||||||||||||||||||
| Event Location: | Potsdam, Germany | ||||||||||||||||||||||||||||||||||||||||||||
| Event Type: | Workshop | ||||||||||||||||||||||||||||||||||||||||||||
| Event Start Date: | 26 November 2024 | ||||||||||||||||||||||||||||||||||||||||||||
| Event End Date: | 27 November 2024 | ||||||||||||||||||||||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||||||||||||||||||||||
| HGF - Program: | Space | ||||||||||||||||||||||||||||||||||||||||||||
| HGF - Program Themes: | Communication, Navigation, Quantum Technology | ||||||||||||||||||||||||||||||||||||||||||||
| DLR - Research area: | Raumfahrt | ||||||||||||||||||||||||||||||||||||||||||||
| DLR - Program: | R KNQ - Communication, Navigation, Quantum Technology | ||||||||||||||||||||||||||||||||||||||||||||
| DLR - Research theme (Project): | R - Ionosphere | ||||||||||||||||||||||||||||||||||||||||||||
| Location: | Neustrelitz | ||||||||||||||||||||||||||||||||||||||||||||
| Institutes and Institutions: | Institute for Solar-Terrestrial Physics > Space Weather Observation | ||||||||||||||||||||||||||||||||||||||||||||
| Deposited By: | Semmling, Dr. Maximilian | ||||||||||||||||||||||||||||||||||||||||||||
| Deposited On: | 16 Dec 2024 14:39 | ||||||||||||||||||||||||||||||||||||||||||||
| Last Modified: | 19 Dec 2025 15:07 |
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