Authors :
Timi V. Nagberi; Iyemeh Uchendu
Volume/Issue :
Volume 11 - 2026, Issue 1 - January
Google Scholar :
https://tinyurl.com/54e2cywb
Scribd :
https://tinyurl.com/ybft63hv
DOI :
https://doi.org/10.38124/ijisrt/26jan229
Note : A published paper may take 4-5 working days from the publication date to appear in PlumX Metrics, Semantic Scholar, and ResearchGate.
Abstract :
Land Mobile Satellite Service (LMSS) terminals operating over geostationary (GEO) links experience persistent
challenges in maintaining pointing continuity under vehicular motion, urban shadowing, and signal blockage. Conventional
GNSS/INS-only predictors suffer from drift during outages, while monopulse tracking introduces prohibitive RF complexity
for compact mobile terminals. This paper presents a low-complexity, comparator-assisted tracking architecture for real-
time realignment of vehicle-mounted GEO LMSS terminals. The proposed system integrates a four-facet power-difference
comparator that supplies residual pointing correction to an Extended Kalman Filter (EKF)–assisted estimator. The EKF
fuses GNSS and inertial measurements to jointly estimate attitude, Doppler, and bias states, while a dual-axis PID controller
performs coarse antenna actuation. A hysteretic beam-selection logic stabilizes sector handover, and an adaptive
frequency/phase-locked loop (FLL/PLL) hybrid preserves carrier lock under rapid signal-to-noise ratio (SNR) fluctuations.
The entire tracking loop is formulated in unified state-space form, enabling analytical derivation of stability limits and
tuning laws. The architecture achieves reduced realignment latency and improved pointing robustness without the
calibration overhead of monopulse systems, making it well suited for small S-band LMSS terminals operating in dynamic
environments.
Keywords :
Land Mobile Satellite Service, GEO Tracking, EKF, Comparator Tracking, Antenna Realignment, Satellite-on-the- Move.
References :
- T. Pratt and J. E. Allnutt, Satellite Communications, 3rd ed. Hoboken, NJ, USA: Wiley, 2019.
- G. Maral and M. Bousquet, Satellite Communications Systems, 6th ed. Hoboken, NJ, USA: Wiley, 2020.
- S. Granet et al., “Satellite-on-the-move antenna systems: Design challenges and trends,” IEEE Antennas Propag. Mag., vol. 61, no. 3, pp. 36–48, 2019.
- H. Lin et al., “Closed-loop and open-loop tracking techniques for mobile satellite receivers,” IEEE Trans. Veh. Technol., vol. 66, no. 8, pp. 6892–6903, 2017.
- T. Jin et al., “Hybrid carrier tracking for high-dynamics satellite communication,” IEEE Commun. Lett., vol. 24, no. 5, pp. 1123–1127, 2020.
- X. Wang et al., “Beam tracking for LEO satellite communication systems,” IEEE Trans. Wireless Commun., vol. 23, no. 2, pp. 1345–1357, 2024.
- H. Rouzegar et al., “Satellite tracking using Doppler shift estimation,” IET Radar, Sonar & Navigation, vol. 11, no. 9, pp. 1410–1418, 2017.
- Q. Liu et al., “AI-assisted antenna tracking in satellite communication,” IEEE Access, vol. 7, pp. 112345–112357, 2019.
- F. Li et al., “Doppler mitigation techniques in mobile satellite systems,” IEEE Syst. J., vol. 14, no. 4, pp. 5234–5245, 2020.
- B. Ekengwu et al., “Performance metrics for mobile satellite tracking,” Int. J. Satell. Commun. Netw., vol. 40, no. 2, pp. 155–170, 2022.
Land Mobile Satellite Service (LMSS) terminals operating over geostationary (GEO) links experience persistent
challenges in maintaining pointing continuity under vehicular motion, urban shadowing, and signal blockage. Conventional
GNSS/INS-only predictors suffer from drift during outages, while monopulse tracking introduces prohibitive RF complexity
for compact mobile terminals. This paper presents a low-complexity, comparator-assisted tracking architecture for real-
time realignment of vehicle-mounted GEO LMSS terminals. The proposed system integrates a four-facet power-difference
comparator that supplies residual pointing correction to an Extended Kalman Filter (EKF)–assisted estimator. The EKF
fuses GNSS and inertial measurements to jointly estimate attitude, Doppler, and bias states, while a dual-axis PID controller
performs coarse antenna actuation. A hysteretic beam-selection logic stabilizes sector handover, and an adaptive
frequency/phase-locked loop (FLL/PLL) hybrid preserves carrier lock under rapid signal-to-noise ratio (SNR) fluctuations.
The entire tracking loop is formulated in unified state-space form, enabling analytical derivation of stability limits and
tuning laws. The architecture achieves reduced realignment latency and improved pointing robustness without the
calibration overhead of monopulse systems, making it well suited for small S-band LMSS terminals operating in dynamic
environments.
Keywords :
Land Mobile Satellite Service, GEO Tracking, EKF, Comparator Tracking, Antenna Realignment, Satellite-on-the- Move.