Equipment Specifications & Inspection Methodology

Complete technical documentation for our thermal inspection platform: camera specifications, ground sample distance at operating altitudes, calibration procedures, and how the specifications relate to solar PV thermographic inspection topics addressed by IEC TS 62446-3.

This page is intended for solar O&M engineers, asset managers, and procurement teams evaluating inspection providers. All specifications are from manufacturer datasheets unless otherwise noted. We distinguish between manufacturer specs, calculated values, and our operational parameters.

Primary Equipment

ParameterSpecificationSource
Sensor TypeUncooled VOx microbolometerManufacturer
Resolution640×512 radiometricManufacturer
Pixel Pitch12 µmManufacturer
Focal Length13mmManufacturer
Spectral Range8-14 µm (LWIR)Manufacturer
NETD≤50 mK @ 30°C (typical)Manufacturer
Temperature Accuracy±3°C or ±3% of reading (whichever greater)Manufacturer
Accuracy Environment−20°C to +60°C environmentManufacturer
Accurate Measurement Distance2–20 m accurate measurement distanceManufacturer
Radiometric OutputR-JPEG with full per-pixel temperature matrix (14-bit)Manufacturer
Frame Rate30 HzManufacturer

What NETD Means in Practice

The sensor's published NETD describes thermal sensitivity under specified conditions; it does not establish individual-cell or incipient-defect detection in delivered field data.

Important Caveats

  • Accuracy valid only within stated environmental range; performance outside range is unspecified
  • Quantitative temperature readings require 2–20 m standoff; beyond 20 m treat values as qualitative unless validated
  • Thermal sensitivity (NETD) degrades at elevated ambient temperatures

RGB Visual Camera

Resolution: 50 MP (4K video)

Sensor: 1" CMOS with mechanical shutter

Output: DNG (RAW) + JPEG with EXIF GPS metadata

The RGB camera provides visual documentation of physical damage, soiling patterns, vegetation encroachment, and installation issues. Thermal and RGB images are captured simultaneously with aligned fields of view for defect correlation.

RTK GPS Positioning

ParameterSpecification
Manufacturer Camera Position (Horizontal, RTK Fix)1 cm + 1 ppm
Manufacturer Camera Position (Vertical, RTK Fix)1.5 cm + 1 ppm
RTK NetworkRTK corrections via NTRIP when network and cellular conditions support a fix
Fallback Mode±1–1.5 m GPS fallback if RTK signal lost
Practical impact: The manufacturer specification describes camera position under RTK Fix, not delivered defect-location accuracy. Clients can open the georeferenced visual and radiometric thermal layers in their own GIS; we do not issue per-module diagnoses.
Correction delivery: RTK corrections can be delivered through NTRIP when cellular and network conditions support a fix. Fix status and project evidence are documented; no delivered absolute-accuracy claim is inferred from RTK alone.

Aircraft Operating Limits

Operating Temperature

−10°C to +40°C

Wind Resistance (Manufacturer)

27 mph (12 m/s) maximum

Operational Limit (Thermal Inspections)

14 mph (6 m/s) — our operational ceiling for thermal inspections

Flight Time

~38 min (varies with payload and conditions)

Aircraft operating temperature range is DIFFERENT from thermal camera accuracy range Wind resistance affects radiometric measurement accuracy (wind cools targets) Battery performance degrades in extreme cold

Ground Sample Distance (GSD) at Operating Altitudes

Thermal GSD vs. Altitude

GSD Formula

GSD = (H x pixel_pitch) / focal_length

Where H = altitude AGL, pixel_pitch = 12 µm, focal_length = 13 mm

AltitudeGSDpx/cell (~6 in. / 156 mm)px/cell (~3 in. / 78 mm half-cut)Illustrative capture-detail tier
49 ft (15m)1.4 cm/px11.35.711.3 px/cell
66 ft (20m)1.8 cm/px8.54.28.5 px/cell
82 ft (25m)2.3 cm/px6.83.46.8 px/cell
98 ft (30m)2.8 cm/px5.62.85.6 px/cell
131 ft (40m)3.7 cm/px4.22.14.2 px/cell
164 ft (50m)4.6 cm/px3.41.73.4 px/cell
197 ft (60m)5.5 cm/px2.81.42.8 px/cell
246 ft (75m)6.9 cm/px2.31.12.3 px/cell

This table is planning math, not a delivered-resolution promise. The aircraft records 640×512 radiometric thermal data; thermal resolution depends on flight altitude, lens choice, and capture geometry.

Practical Note on Half-Cut Cells

Modern panels increasingly use half-cut cells (~3 in. / 78 mm). These require lower altitudes for the same pixel-per-cell count. At 98 ft (30m) AGL, a half-cut cell gets only ~2.8 pixels across—below the detailed mode threshold. For half-cut-cell planning, lower altitude increases pixel sampling; project geometry and safety constraints determine the flight plan. Pixel counts do not establish an individual-cell diagnosis.

Measurement Distance Constraint

The Autel 640T specifies accurate temperature measurement at 7–65 ft (2–20m) standoff distance. At flight altitudes above 65 ft (20m), absolute temperature readings should be treated as qualitative unless field-validated. For commissioned solar screening, we compare relative surface-temperature differences and document the reference selection. Relative differences (Tdefect - Tref) remain valid at higher altitudes because the atmospheric attenuation affects both measurements equally. Anomalies flagged at altitude are confirmed with low-altitude verification passes when quantitative temperature values are required.

Calibration & Maintenance Schedule

ActivityFrequencyMethod
Factory CalibrationAnnualReturn to manufacturer. Blackbody reference sources, NIST-traceable. Certificate of calibration provided.
Field VerificationQuarterlyCheck against portable blackbody reference target at known temperatures. Verify reading is within manufacturer's stated accuracy (±3°C or ±3% of reading (whichever greater)).
Commissioned-Scope Equipment ChecksAs specified in the commissioned checklistAvailable checks include NUC (Non-Uniformity Correction), lens-cover cycling, stable-image review, and ambient capture-context notes.
Lens CleaningAs specified in the commissioned equipment checklistThe commissioned checklist can call for visual inspection of the Germanium lens and cleaning with lens-safe solution only when contamination is present; the Ge window is factory-coated and unnecessary contact risks surface damage. Dust, fingerprints, or organic residue on the Ge window degrade thermal transmission and introduce measurement error.
Aircraft RTK StatusBefore survey captureManufacturer RTK state describes camera-position metadata; it does not establish delivered finding accuracy.

Ask which equipment records are available for your scope. A commissioned deliverable identifies any manufacturer or field records included with that project.

How Documented Field Practices Relate to the Framework's Inspection Topics

Environmental Conditions

The commissioned capture plan defines environmental data-quality gates. We log the applicable conditions before and during the flight and report departures from the plan.

Inspection topicDocumented project procedureVerification Method
Plane-of-array irradiance ≥600 W/m²Minimum 600 W/m²; preferred ≥700 W/m². Flight aborted if irradiance drops below 600 W/m² for more than 2 minutes.Irradiance verified via site sensor data or reference irradiance sources, logged with the flight record.
Irradiance stability (<10% variation/min)Flights scheduled during cloud-free windows. Data from intermittent cloud periods flagged and reviewed before inclusion.Irradiance verified via site sensor data or reference irradiance sources, logged with the flight record. Post-flight QA rejects frames captured during irradiance dips.
Wind speed ≤22 mph (10 m/s)We target ≤11 mph (5 m/s) as the stated data-quality target for this workflow. Wind speed is logged; marginal or aborted conditions are governed by the commissioned capture plan.On-site anemometer. Wind speeds above 11 mph (5 m/s) are noted as a condition in the report because convective cooling reduces apparent ΔT.
Modules under normal operating loadConfirmed with site operator that all strings and inverters are energized before survey begins. Any known offline strings are documented.Pre-flight coordination with site O&M team. Inverter status logged at survey start.

Camera & Resolution Requirements

Inspection characteristicEquipment specification
Radiometric thermal camera640x512 radiometric sensor; full per-pixel temperature data stored in R-JPEG format. 14-bit thermal data, not visual-only palette overlay.
NETD ≤0.1 K (recommended)≤50 mK (0.05 K) manufacturer-listed NETD
≥5x5 px/cell (detailed mode)Achieved at ≤98 ft (30m) AGL for ~6 in. (156 mm) cells. See GSD table for altitude/resolution tradeoffs. We confirm cell dimensions with the client and select flight altitude accordingly.
≥3x3 px/cell (simplified mode)Achieved at ≤164 ft (50m) AGL for ~6 in. (156 mm) cells. Used for high-altitude screening passes on large arrays before targeted low-altitude detail passes.
View angle ≤60° from perpendicularWe target ≤30° from perpendicular (nadir or near-nadir) to minimize emissivity variation and reflected apparent temperature. Flight path planned to maintain consistent viewing geometry across the array. Module tilt angle factored into flight planning.

Flight Pattern & Coverage

Systematic Grid Survey

  • Pattern: Parallel flight lines aligned with tracker rows or fixed-tilt row orientation
  • Forward Overlap: ≥70% (thermal), ≥80% (RGB) — adds repeat observations along the flight path
  • Side Overlap: ≥60% (thermal), ≥70% (RGB) — ensures full coverage between adjacent flight lines
  • Speed: 7–11 mph (3–5 m/s) depending on altitude and GSD target. Slower speed = less motion blur in thermal frames.

Image Capture

  • Trigger: Distance-based (not time-based) to maintain consistent overlap regardless of wind-induced speed variations
  • Orientation: Camera nadir (pointing straight down) or tilted to match module plane-of-array angle for perpendicular viewing
  • Thermal/RGB relationship: Capture streams are not assumed to be paired at identical timestamps
  • Metadata: Available pose and timestamp records are retained and their limits documented

Why High Overlap Matters

Higher forward overlap increases repeat observations where frame coverage overlaps. Reviewers can compare transient artifacts such as passing shadows across adjacent frames, while thermal signatures remain investigation targets for ground verification. Absolute coordinate accuracy is stated only when measured for the project.

Data Processing Pipeline

1

Ingest & Quality Gate

Raw R-JPEG thermal frames, RGB images, flight logs, and irradiance-source data are ingested. Automated QA rejects frames captured during irradiance dips (<600 W/m²), excessive motion blur, or RTK signal loss. Typically 5-15% of frames are rejected during QA depending on conditions.

2

Radiometric Orthomosaic Generation

Thermal frames are stitched into a georeferenced orthomosaic using photogrammetric processing. Crucially, this is a radiometric mosaic — the per-pixel temperature values are preserved through the stitching process, not averaged into visual-only palettes. The result is a georeferenced GeoTIFF containing radiometric apparent-temperature data, documented processing, and disclosed quality limits.

3

Anomaly Detection & Classification

Temperature differences (ΔT) between suspected anomalies and adjacent healthy reference modules are calculated and normalized to 1000 W/m² standard irradiance using the formula:

ΔTn = (Tdefect - Tref) x (1000 / Gmeas)

Observed signatures are labeled by pattern and confidence, then separated as confirmed or suspected for ground verification. Pattern labels are not root-cause diagnoses. See our IEC TS 62446-3 methodology page for the reporting framework and priority bins.

4

Peer Review & Validation

Every anomaly is manually reviewed against the paired RGB image to confirm physical plausibility. Suspected false positives (bird droppings, temporary shading, reflections) are flagged and downgraded or removed. For suspected transient anomalies, the repeat-frame redundancy from our 70%+ overlap is used to confirm persistence.

5

Deliverable Generation

Final outputs are generated in multiple formats for different stakeholders. See Deliverable Formats below.

Deliverable Formats

GeoTIFF Thermal Orthomosaic

Georeferenced thermal map of the full site with preserved radiometric data. Compatible with QGIS, ArcGIS, and most asset management GIS systems.

CRS: UTM Zone 14N (EPSG:32614) for orthomosaics; WGS84 (EPSG:4326) for point data

CSV Anomaly Log

Row-level defect records with GPS coordinates, normalized ΔT, severity classification, anomaly type, and image references. Designed for direct import into CMMS platforms.

See CSV schema documentation for field definitions.

KML/KMZ Field Maps

Pin-drop anomaly locations color-coded by severity. Designed for field crew tablets. Tap a pin to see anomaly type, ΔT, severity, and a thermal thumbnail.

Compatible with Google Earth, Avenza Maps, and standard GPS navigation apps

PDF Inspection Report

Human-readable report with executive summary, findings by severity, thermal+RGB image pairs for each anomaly, and inspection conditions metadata. Format varies by service tier.

Enterprise tier includes a documented project-method appendix with available calibration records.

Data Interoperability

All deliverables use open, standard formats. No proprietary viewer required. For integration with specific asset management platforms (PowerFactors, Raptor Maps, etc.), we can adjust field mappings and export schemas. See our data interoperability page for details.

Quality Assurance

Every inspection passes through these QA gates before deliverables are released to the client.

Environmental-condition record: Irradiance verified via site sensor data or reference irradiance sources, logged with the flight record. Wind speed, ambient temperature, and cloud conditions logged.

Spatial coverage: Orthomosaic checked against site plan for gaps. Any uncovered areas noted in the report with reason (access restriction, tracker in stow, etc.).

RTK positioning: RTK Fix percentage for the survey is reported. Frames captured during RTK Float or standalone GPS mode are flagged with degraded position accuracy.

False positive review: Every flagged anomaly verified against RGB imagery and repeat frames. Transient artifacts removed. Borderline cases are included with a reduced confidence notation rather than silently dropped.

Normalization check: ΔT values are spot-checked against raw radiometric data to confirm normalization formula was applied correctly. Reference temperature selection is checked against the documented project method and the selected comparison modules are recorded.

Accuracy Disclosure

Temperature measurement accuracy: ±3°C or ±3% of reading (whichever greater), valid within a −20°C to +60°C environment; accurate measurement distance 2–20 m.

IEC 62446-3 anomaly classifications assume ≥600 W/m² plane-of-array irradiance with stable conditions

Temperature measurement accuracy: ±3°C or ±3% of reading (whichever greater), valid within −20°C to +60°C environment

Quantitative readings assume 2–20 m measurement distance; beyond this, treat values as qualitative

What This Means for Your Reports

Our defect classification relies on relative temperature differences (ΔT between anomaly and reference), not absolute temperature readings. Relative measurements are more robust than absolute values because atmospheric and environmental effects largely cancel out. The High Thermal Sensitivity absolute accuracy specification is relevant for specific engineering analyses (e.g., comparing measured module temperature to modeled predictions) but does not directly affect ΔT-based anomaly classification.

Related Technical Resources

Questions About Our Equipment or Methodology?

We welcome technical questions from solar engineers, asset managers, and procurement teams. If you want to see sample deliverables or discuss how our methodology applies to your specific site configuration, reach out.

Based in Hale Center, TX. Serving the Texas Panhandle, South Plains, and ERCOT footprint. No travel fees within 40 miles.