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Flight-test sensing and data analysis for paraglider, paramotor and kite developers

I build the sensors, log the data in flight and turn it into numbers you can base development decisions on.

Book a free 30-minute call

Available from mid-November 2026 · on-site in Germany, Austria and Switzerland

What I build

Low-speed air data

True airspeed and angle of attack at the low flight speeds of soft wings.

Canopy internal pressure

Pressure sensing inside the wing.

Pilot-input measurement

Control forces and control travel, measured in flight.

Synchronised logging

All channels logged together with IMU, GNSS and video, so every manoeuvre can be analysed across sensors.

What I deliver

In-flight calibration

Calibration of airspeed and flow-angle sensors from flight data.

Wind and installation errors

Estimation of wind and sensor installation errors with an extended Kalman filter and smoother.

Glide polar and trim

Glide-polar and trim analysis from the measured flights.

System identification

Flight-dynamics models identified from flight data.

Test reports

Reports written for development decisions: what was measured, how reliable it is, and what it means for the wing.

Track record

SkySails, 2020–2024

Wind-field estimators for large traction kites.

ParaDoc, 2026

My own sensor hardware, flown on my paramotor: working EGT monitoring and alarm; acoustic and vibration diagnostics in development.

See ParaDoc →

Paragliding variometer with sensor fusion, 2014–2015

Nonlinear estimation, first-principles modelling, data acquisition and test flights.

Research

PhD on economic nonlinear model predictive control (NMPC) for the LHC cryogenics at CERN; NMPC and state estimation for wind turbines at IAV.

Pilot

1,000+ hours paragliding, 500+ hours gliding.

Contact

rafal@noga.es
Phone: +49 175 617 6792

Available from mid-November 2026, on-site in Germany, Austria and Switzerland.

Planning a flight-test campaign?

A 30-minute call is enough to see what should be measured and how.

Book a free 30-minute call →

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