Ram Kumar Vankadara

Mr. Ram Kumar Vankadara

E.C.E, Koneru Lakshmaiah Education Foundation, Vijayawada, India
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Research Focus & Metrics

Academic Career Length

5Years (2022-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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29 January 2022 in Remote Sensing
Verified
Journal Article
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RVRam Kumar Vankadara
Ram Kumar Vankadara
SPSampad Kumar Panda
Sampad Kumar Panda
Christine Amory-MazaudierChristine Amory-Mazaudier
Christine Amory-Mazaudier
RFRolland Fleury
Rolland Fleury
VDVenkata Ratnam Devanaboyina
Venkata Ratnam Devanaboyina
GSGopi Krishna Seemala
Gopi Krishna Seemala
Scintillation due to ionospheric plasma irregularities remains a challenging task for the space science community as it can severely threaten the dynamic systems relying on space-based navigation services. In the present paper, we probe the ionospheric current and plasma irregularity characteristics from a latitudinal arrangement of magnetometers and Global Navigation Satellite System (GNSS) stations from the equator to the far low latitude location over the Indian longitudes, during the severe space weather events of 6–10 September 2017 that are associated with the strongest and consecutive solar flares in the 24th solar cycle. The night-time influence of partial ring current signatures in ASYH and the daytime influence of the disturbances in the ionospheric E region electric currents (Diono) are highlighted during the event. The total electron content (TEC) from the latitudinal GNSS observables indicate a perturbed equatorial ionization anomaly (EIA) condition on 7 September, due to a sequence of M-class solar flares and associated prompt penetration electric fields (PPEFs), whereas the suppressed EIA on 8 September with an inverted equatorial electrojet (EEJ) suggests the driving disturbance dynamo electric current (Ddyn) corresponding to disturbance dynamo electric fields (DDEFs) penetration in the E region and additional contributions from the plausible storm-time compositional changes (O/N2) in the F-region. The concurrent analysis of the Diono and EEJ strengths help in identifying the pre-reversal effect (PRE) condition to seed the development of equatorial plasma bubbles (EPBs) during the local evening sector on the storm day. The severity of ionospheric irregularities at different latitudes is revealed from the occurrence rate of the rate of change of TEC index (ROTI) variations. Further, the investigations of the hourly maximum absolute error (MAE) and root mean square error (RMSE) of ROTI from the reference quiet days’ levels and the timestamps of ROTI peak magnitudes substantiate the severity, latitudinal time lag in the peak of irregularity, and poleward expansion of EPBs and associated scintillations. The key findings from this study strengthen the understanding of evolution and the drifting characteristics of plasma irregularities over the Indian low latitudes.

1 November 2023 in IEEE Transactions on Plasma Science
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Journal Article
Closed access
RVRam Kumar Vankadara
Ram Kumar Vankadara
MMMefe Moses
Mefe Moses
M.I.H. SiddiquiM.I.H. Siddiqui
M.I.H. Siddiqui
Kutubuddin AnsariKutubuddin Ansari
Kutubuddin Ansari
SPSampad Kumar Panda
Sampad Kumar Panda
Forecasting ionospheric total electron content (TEC) has been of great interest among ionospheric researchers and radio propagation scientists as it critically affects the operation of dynamic technological systems relying on space-based radio propagation. In this context, this article attempts to forecast ionospheric TEC using a bi-long short-term memory (Bi-LSTM) deep learning neural network model at a low-latitude location (KLEF Campus; geographic 16 $^{\circ}$ 26’N, 80 $^{\circ}$ 37’E; dip 22 $^{\circ}$ 11’) in Guntur, India. We employed the TEC observables from a specialized global navigation satellite system (GNSS) ionospheric scintillation and TEC monitoring (GISTM) receiver as input data for the deep learning model. To include external ionospheric characteristics, geomagnetic and solar indices (Kp, ap, F10.7, sunspot number (SSN), and Sym-H) were also considered whose individual effects are realized before incorporating them in the model. The performance of the Bi-LSTM model was compared with the conventional LSTM, time-series autoregressive integrated moving average (ARIMA), the latest edition of global empirical international reference ionosphere (IRI-2020) models, and the TEC extracted from hourly global ionospheric maps (GIMs) using statical metrics like root-mean-square error (RMSE), maximum absolute error (MAE), and R error measurements. The Bi-LSTM model showed a low RMSE value of 7.73 TEC unit (TECU), while the LSTM and ARIMA models had values of 8.16 and 8.39 TECU, respectively. The Bi-LSTM model also had the highest correlation ( R $=$ 0.962), followed by the LSTM ( R $=$ 0.957) and ARIMA ( R $=$ 0.956). The day-to-day performance of the TEC forecast was evaluated for quiet and disturbed days, confirming a substantial performance irrespective of geomagnetic activity. Further assessment of the model performance at other latitudes in a wider range of the Indian longitude sector may provide more insight into its predictability for regional deployment.

13 October 2023 in Remote Sensing
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Journal Article
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RVRam Kumar Vankadara
Ram Kumar Vankadara
PJPunyawi Jamjareegulgarn
Punyawi Jamjareegulgarn
GSGopi Krishna Seemala
Gopi Krishna Seemala
M.I.H. SiddiquiM.I.H. Siddiqui
M.I.H. Siddiqui
SPSampad Kumar Panda
Sampad Kumar Panda
The equatorial plasma bubbles (EPBs) are depleted plasma density regions in the ionosphere occurring during the post-sunset hours, associated with the signal fading and scintillation signatures in the trans-ionospheric radio signals. Severe scintillations may critically affect the performance of dynamic systems relying on global navigation satellite system (GNSS)-based services. Furthermore, the occurrence of scintillations in the equatorial and low latitudes can be triggered or inhibited during space weather events. In the present study, the possible presence of the EPBs during the geomagnetic storm periods under the 25th solar cycle is investigated using the GNSS-derived total electron content (TEC) depletion characteristics at a low-latitude equatorial ionization anomaly location, i.e., KL University, Guntur (Geographic 16°26′N, 80°37′E and dip 22°32′) in India. The detrended TEC with a specific window size is used to capture the characteristic depletion signatures, indicating the possible presence of the EPBs. Moreover, the TEC depletions, amplitude (S4) and phase scintillation (σφ) indices from multi-constellation GNSS signals are probed to verify the vulnerability of the signals towards the scintillation effects over the region. Observations confirm that all GNSS constellations witness TEC depletions between 15:00 UT and 18:00 UT, which is in good agreement with the recorded scintillation indices. We report characteristic depletion depths (22 to 45 TECU) and depletion times (28 to 48 min) across different constellations confirming the triggering of EPBs during the geomagnetic storm event on 23 April 2023. Unlikely, but the other storm events evidently inhibited TEC depletion, confirming suppressed EPBs. The results suggest that TEC depletions from the traditional geodetic GNSS stations could be used to substantiate the EPB characteristics for developing regional as well as global scintillation mitigation strategies.

10 May 2024 in Remote Sensing
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RVRam Kumar Vankadara
Ram Kumar Vankadara
NDNirvikar Dashora
Nirvikar Dashora
SPSampad Kumar Panda
Sampad Kumar Panda
JDJ R K Kumar Dabbakuti
J R K Kumar Dabbakuti
The equatorial post-sunset ionospheric irregularities induce rapid fluctuations in the phase and amplitude of global navigation satellite system (GNSS) signals which may lead to the loss of lock and can potentially degrade the position accuracy. This study presents a new analysis of L-band scintillation from a low latitude station at Guntur (Geographic 16.44°N, 80.62°E, dip 22.18°), India, for the period of 18 months from August 2021 to January 2023. The observations are categorized either in the medium Earth-orbiting (MEO) or geosynchronous orbiting (GSO) satellites (GSO is considered as a set of the geostationary and inclined geosynchronous satellites) for L1, L2, and L5 signals. The results show a higher occurrence of moderate (0.5 < S4 ≤ 0.8) and strong (S4 > 0.8) scintillations on different signals from the MEO compared to the GSO satellites. Statistically, the average of peak S4 values provides a higher confidence in the severity of scintillations on a given night, which is found to be in-line with the scintillation occurrences. The percentage occurrence of scintillation-affected satellites is found to be higher on L1 compared to other signals, wherein a contrasting higher percentage of affected satellites over GSO than MEO is observed. While a clear demarcation between the L2/L5 signals and L1 is found over the MEO, in the case of GSO, the CCDF over L5 is found to match mostly with the L1 signal. This could possibly originate from the space diversity gain effect known to impact the closely spaced geostationary satellite links. Another major difference of higher slopes and less scatter of S4 values corresponding to L1 versus L2/L5 from the GSO satellite is found compared to mostly non-linear highly scattered relations from the MEO. The distribution of the percentage of scintillation-affected satellites on L1 shows a close match between MEO and GSO in a total number of minutes up to ~60%. However, such a number of minutes corresponding to higher than 60% is found to be larger for GSO. Thus, the results indicate the possibility of homogeneous spatial patterns in a scintillation distribution over a low latitude site, which could originate from the closely spaced GSO links and highlight the role of the number of available satellites with the geometry of the links, being the deciding factors. This helps the ionospheric community to develop inter-GNSS (MEO and GSO) operability models for achieving highly accurate positioning solutions during adverse ionospheric weather conditions.

22 September 2025 in Advances In Space Research
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Journal Article
Closed access
SPSampad Kumar Panda
Sampad Kumar Panda
SRSiva Sai Kumar Rajana
Siva Sai Kumar Rajana
CVChiranjeevi G. Vivek
Chiranjeevi G. Vivek
RVRam Kumar Vankadara
Ram Kumar Vankadara
PJPunyawi Jamjareegulgarn
Punyawi Jamjareegulgarn