Comprehensive inspection

IEC 62446-3 compliant nadir thermal and RGB capture for module-level anomaly detection.

Environmental requirements

ParameterRequirement
POA irradiance600 W/m² minimum — photograph pyranometer before and after flight
SkyClear to partially cloudy — no cloud shadow over the field during capture
Time of day10:00 – 15:00 local solar time
Wind15 km/h max
Plant statusEnergized and under load for at least 30 min before flight

Flight parameters

ParameterValue
GSD (IR)3.0 cm/px
GSD (RGB)Under 1.0 cm/px (automatic at IR altitude)
Front overlap80%
Side overlap60%
Max speed2.0 m/s
Planning sensorIR camera FOV — not RGB. Using RGB causes IR data gaps at module edges.
AltitudeTerrain follow or RTK MSL

Flight path by site type

Tracker sites: N-S snake (crab fly) along tracker rows. Account for tracker max tilt height in altitude calculation.

Fixed-tilt ground mount: fly perpendicular to the module row orientation.

Rooftop: fly perpendicular to the dominant module row orientation. Adjust pattern to cover the roof footprint — multiple short legs may be needed for irregular shapes.

Camera settings — IR thermal

SettingValue
UHR modeOFF
Resolution640 x 512 px (native)
PaletteIronbow or White-Hot — do not change mid-mission
Emissivity0.95
GainLow Range
Radiometric outputEnabled (RJPEG or TIFF) — mandatory
FFCShutter every 3 min
Capture interval0.7s (M3T)

Camera settings — RGB

SettingValue
Shutter speed1/800s minimum
ISO100 – 400
White balanceDaylight — not Auto
FormatJPEG max quality
SyncSimultaneous with IR

Gimbal and orientation

SettingValue
Camera orientationSide-on (90 deg rotated) — parallel to module long axis
Gimbal pitchNormal to module surface — adjust with tracker angle
Glare mitigation5 – 10 deg tilt from normal if needed; never exceed 30 deg
HeadingConstant throughout mission

Tracker strategy

Time of dayTracker faceDrone heading
Morning (before solar noon)EastCamera faces West
Afternoon (after solar noon)WestCamera faces East

Monitor tracker angle during flight and adjust gimbal pitch to maintain full module face visibility.

Key rules

  • Plan on the IR sensor FOV, not RGB. This is the most common cause of data rejection.
  • Speed limit is strict — 2.0 m/s. Reduce to 1.5 m/s if mid-flight spot-check shows soft module edges.
  • All IR images must be radiometric (RJPEG/TIFF). Non-radiometric JPEGs cannot be processed.
  • Irradiance proof — photograph your pyranometer at start and end of each flight segment.