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arxiv: 2604.06444 · v1 · submitted 2026-04-07 · 📡 eess.SP · cs.NI

Real-World LoRaWAN Performance and Propagation Modeling Using UAV, Helikite, and Vehicle-Based Measurements

Pith reviewed 2026-05-10 18:21 UTC · model grok-4.3

classification 📡 eess.SP cs.NI
keywords LoRaWANpropagation modelingUAV measurementshelikiteRSSISNRlog-distance path lossaerial networks
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The pith

Helikite measurements at 150-300 meters yield more consistent LoRaWAN links than drone or ground-vehicle tests across the same sites.

A machine-rendered reading of the paper's core claim, the machinery that carries it, and where it could break.

The paper compares LoRaWAN signal reception using a ground vehicle, a drone at 50 meters, and a helikite at steady altitudes of 150 and 300 meters at two AERPAW testbed locations. It tracks RSSI and SNR against distance and spreading factor, then fits a log-distance path-loss model to the vehicle data covering rural and urban non-line-of-sight conditions. The central observation is that the helikite's fixed high position produces the least variable links, while movement and terrain effects increase variability for the drone and vehicle. This comparison is meant to inform planning for aerial wireless networks that rely on LoRaWAN.

Core claim

Field data collected with three platforms show that a helikite at fixed high altitude produces the most reliable and consistent LoRaWAN reception, while a moving drone at 50 m and a ground vehicle exhibit greater variability from motion, obstructions, and terrain-induced multipath; a log-distance path-loss model fitted to the vehicle measurements quantifies propagation under mixed rural-urban NLOS conditions.

What carries the argument

Comparative RSSI and SNR measurements versus distance, together with a fitted log-distance path-loss model applied to ground-vehicle data.

If this is right

  • Adaptive spreading-factor selection becomes more critical for mobile platforms than for fixed high-altitude ones.
  • Network planners can use the fitted log-distance parameters to estimate coverage when ground-level nodes interact with aerial gateways.
  • Helikite-style platforms may reduce the need for frequent retransmissions in LoRaWAN deployments that tolerate higher altitudes.

Where Pith is reading between the lines

These are editorial extensions of the paper, not claims the author makes directly.

  • If the stability advantage holds, helikites could serve as low-cost relays for extending LoRaWAN range in areas with variable terrain.
  • The variability patterns suggest that drone-based LoRaWAN surveys would need shorter flight segments or higher sampling rates to match helikite reliability.

Load-bearing premise

The AERPAW testbed sites, chosen altitudes, and vehicle routes are representative enough that the relative performance ordering and the fitted model parameters apply to other environments.

What would settle it

Repeating the same three-platform experiment at a new rural or suburban site and finding that the drone or vehicle links show lower variability than the helikite at 150-300 m would falsify the consistency claim.

Figures

Figures reproduced from arXiv: 2604.06444 by \.Ismail G\"uven\c{c}, Mihail L. Sichitiu, \"Ozg\"ur \"Ozdemir, Sergio Vargas Villar, Simran Singh.

Figure 1
Figure 1. Figure 1: AERPAW vehicle platforms used in the experiments: small AERPAW multicopter (SAM) and helikite. [PITH_FULL_IMAGE:figures/full_fig_p002_1.png] view at source ↗
Figure 2
Figure 2. Figure 2: Predefined drone flight path used during [PITH_FULL_IMAGE:figures/full_fig_p002_2.png] view at source ↗
Figure 3
Figure 3. Figure 3: Lab experiment areas and maps: (a) Deployment of LoRaWAN gateways CC2 and CC3 in NC State’s ()() ( [PITH_FULL_IMAGE:figures/full_fig_p004_3.png] view at source ↗
Figure 4
Figure 4. Figure 4: Trade-off between range and data rate for [PITH_FULL_IMAGE:figures/full_fig_p004_4.png] view at source ↗
Figure 5
Figure 5. Figure 5: Vehicle trajectory and gateway locations [PITH_FULL_IMAGE:figures/full_fig_p005_5.png] view at source ↗
Figure 6
Figure 6. Figure 6: Car experiment results: (a) RSSI CDF per gateway, (b) SNR CDF per gateway, (c) SNR vs distance by () () () [PITH_FULL_IMAGE:figures/full_fig_p007_6.png] view at source ↗
Figure 7
Figure 7. Figure 7: Helikite experiment results at Lake Wheeler Field (rural LOS): (a) Trajectory and gateway locations () () () [PITH_FULL_IMAGE:figures/full_fig_p008_7.png] view at source ↗
Figure 8
Figure 8. Figure 8: Helikite experiment results (Main Campus, urban LOS): (a) Flight path and gateway locations, (b) RSSI () () () [PITH_FULL_IMAGE:figures/full_fig_p010_8.png] view at source ↗
Figure 9
Figure 9. Figure 9: Drone experiment results at Lake Wheeler Field: (a) Flight path and gateway locations, (b) RSSI CDF () () () [PITH_FULL_IMAGE:figures/full_fig_p012_9.png] view at source ↗
read the original abstract

This paper presents a field-based evaluation of Long Range Wide Area Network (LoRaWAN) signal propagation conducted at two locations within the Aerial Experimentation and Research Platform for Advanced Wireless (AERPAW) testbed: Lake Wheeler Field and NC State University's Centennial Campus. Three distinct transmission platforms were deployed, a ground vehicle, a multirotor drone at 50 meters, and a helikite at a steady altitude of 150 meters and 300 meters approximately. These platforms enabled a comparative study on how altitude, mobility, and terrain influence wireless signal reception across a LoRaWAN gateway network. We analyze received signal strength (RSSI) and signal-to-noise ratio (SNR) as functions of distance and spreading factor (SF). Three complementary metrics are visualized: SNR versus distance with demodulation thresholds, probability of successful reception, and SNR boxplots grouped by distance bins. These plots reveal link degradation patterns and demonstrate the role of adaptive SF selection in maintaining communication reliability. To characterize propagation behavior, we apply a log-distance path loss model to empirical data from the ground vehicle experiment, which encompass both rural and urban non-line-of-sight (NLOS) conditions. Model parameters are optimized through error minimization techniques. Our results show that the helikite platform, due to its stable high-altitude position, provided the most reliable and consistent link performance. Conversely, the drone and vehicle exhibited higher variability due to movement, obstructions, and terrain-induced multipath. These findings demonstrate the influence of platform dynamics and altitude on LoRaWAN reception performance, providing support for future aerial network planning efforts.

Editorial analysis

A structured set of objections, weighed in public.

Desk editor's note, referee report, simulated authors' rebuttal, and a circularity audit. Tearing a paper down is the easy half of reading it; the pith above is the substance, this is the friction.

Referee Report

3 major / 3 minor

Summary. The paper presents field measurements of LoRaWAN performance using three platforms—ground vehicle, drone at 50 m, and helikite at 150-300 m—at two AERPAW testbed sites. It analyzes RSSI and SNR as functions of distance and spreading factor, visualizes metrics like reception probability and boxplots, fits a log-distance path loss model to vehicle data via error minimization, and concludes that the helikite offers the most reliable performance due to its stable altitude while drone and vehicle show higher variability.

Significance. If validated, the empirical comparison of platform effects on LoRaWAN links could inform aerial network deployments for IoT applications. The multi-platform approach and focus on real-world NLOS conditions are positive aspects, though the limited number of sites and lack of statistical rigor reduce the immediate impact.

major comments (3)
  1. [Abstract] Abstract and results sections: No sample sizes, number of packets transmitted, or error bars/confidence intervals are reported for the RSSI/SNR measurements, boxplots, or reception probability curves, preventing quantitative assessment of the variability claims and platform comparisons.
  2. [Propagation modeling] Propagation modeling section: The log-distance path loss model is fitted exclusively to the ground-vehicle dataset using error minimization, with no equivalent parameter estimation, validation, or statistical comparison performed on the drone or helikite data despite their central role in the platform performance conclusions.
  3. [Results and discussion] Results and discussion: The attribution of helikite superiority to stable high altitude (vs. movement and multipath in other platforms) lacks supporting statistical tests (e.g., variance tests or ANOVA on SNR distributions across distance bins) and is based solely on data from two specific AERPAW sites without replication or controls for site-specific terrain effects.
minor comments (3)
  1. [Abstract] Clarify in the abstract and methods whether the helikite operated at both 150 m and 300 m altitudes in separate flights or if these are approximate values.
  2. [Figures] Add sample sizes per distance bin to the SNR boxplots and reception probability figures for better interpretability of the empirical trends.
  3. [Propagation modeling] Include a brief comparison of the fitted path-loss exponent and reference loss to standard LoRaWAN models in the literature.

Simulated Author's Rebuttal

3 responses · 1 unresolved

We thank the referee for the constructive comments, which help strengthen the manuscript. We address each major comment point by point below.

read point-by-point responses
  1. Referee: [Abstract] Abstract and results sections: No sample sizes, number of packets transmitted, or error bars/confidence intervals are reported for the RSSI/SNR measurements, boxplots, or reception probability curves, preventing quantitative assessment of the variability claims and platform comparisons.

    Authors: We agree that sample sizes and measures of variability are important for quantitative assessment. In the revised manuscript, we will report the number of packets transmitted for each platform and experiment, and add error bars or confidence intervals to the RSSI/SNR plots, boxplots, and reception probability curves. revision: yes

  2. Referee: [Propagation modeling] Propagation modeling section: The log-distance path loss model is fitted exclusively to the ground-vehicle dataset using error minimization, with no equivalent parameter estimation, validation, or statistical comparison performed on the drone or helikite data despite their central role in the platform performance conclusions.

    Authors: The log-distance path loss model was applied specifically to the ground-vehicle dataset because it spans both rural and urban NLOS conditions and provides a suitable baseline for propagation characterization. The drone and helikite operate at substantially higher altitudes, which changes the propagation environment (fewer obstructions and multipath effects), so the same model form is not directly comparable without additional modeling assumptions. We will revise the section to explicitly justify this choice and, where the data volume permits, include parameter estimates for the aerial platforms with a brief comparative discussion. revision: partial

  3. Referee: [Results and discussion] Results and discussion: The attribution of helikite superiority to stable high altitude (vs. movement and multipath in other platforms) lacks supporting statistical tests (e.g., variance tests or ANOVA on SNR distributions across distance bins) and is based solely on data from two specific AERPAW sites without replication or controls for site-specific terrain effects.

    Authors: We will add statistical tests (e.g., Levene’s test for equality of variances or ANOVA on SNR values across distance bins) to quantify the platform differences in variability. The experiments were performed only at the two available AERPAW sites (Lake Wheeler Field and Centennial Campus); we will explicitly acknowledge this limitation and its implications for generalizability in the revised discussion. revision: partial

standing simulated objections not resolved
  • Additional replication at other sites or with explicit terrain controls is not feasible, as the measurements were conducted exclusively at the two AERPAW locations using the available testbed infrastructure.

Circularity Check

0 steps flagged

No significant circularity in derivation chain

full rationale

The paper's primary claims regarding helikite superiority in link consistency derive directly from independent empirical measurements of RSSI, SNR, reception probability, and variability across platforms at the AERPAW sites. The log-distance path loss model is fitted exclusively to ground-vehicle data via error minimization and is not used to derive, predict, or substitute for the aerial-platform comparisons. No self-citations, uniqueness theorems, ansatzes, or self-definitional reductions appear in the abstract or described methods that load-bear the central results. The modeling step is a separate characterization of one dataset and does not reduce the comparative findings to its own inputs by construction.

Axiom & Free-Parameter Ledger

1 free parameters · 1 axioms · 0 invented entities

The work rests on one standard empirical model whose two parameters are fitted to the collected ground-vehicle data; no new physical entities are introduced.

free parameters (1)
  • Path-loss exponent and reference loss = Not numerically stated in abstract
    Optimized by error minimization on RSSI measurements from the ground-vehicle experiment in rural and urban NLOS conditions.
axioms (1)
  • domain assumption Log-distance path loss model is a suitable description of signal attenuation in the tested rural and urban NLOS environments
    Invoked when applying the model to empirical data from the ground vehicle.

pith-pipeline@v0.9.0 · 5623 in / 1358 out tokens · 67703 ms · 2026-05-10T18:21:26.807083+00:00 · methodology

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Reference graph

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