Vibrational dynamics of a Morane Saulnier MS.760 Paris Aircraft Wing

Q2 Laser Radar System, for Aviation Applications

Ommatidia Q2 Laser Doppler vibrometer, FMCW

Ground Vibration Testing (GVT) and Maintenance, and Repair and Operation (MRO) activities are essential processes in the lifecycle of an aircraft.
Accurate modal identification and structural validation are required to ensure airworthiness, support structural modifications, and detect early stage damage.

Traditional approaches rely heavily on large accelerometer arrays, complex cabling, and extended setup times, which increase operational cost and limit measurement density >>> Unlike conventional sensor based systems, Q2 requires no accelerometer installation, eliminating mass loading effects, cabling and significantly reducing preparation time.

A dedicated photonic integrated circuit (PICs), analyzes multiple optical channels in parallel, enabling the simultaneous 3D measurement of vibrations and displacements.

Ommatidia´s Q2 Laser Radar provides a contactless, easy to deploy alternative capable of capturing full 3D vibrometry and metrology data using a single mobile unit.

For large scale campaigns, additional Q2 units may be deployed to accelerate acquisition and enable simultaneous multi axis or multi location measurements.

Ommatidia Upgrade & Trade-In Program

Upgrade to Ommatidia’s latest Laser RADAR technology and unlock more capability for your next measurement challenge. Whether you are expanding an existing setup or replacing an older system, we offer tailored upgrade options with discounts of up to 40%.

If you are currently using another manufacturer’s system, send us your model and measurement requirements. We will review your trade-in possibilities, identify the best Ommatidia configuration, and outline a practical upgrade path for your team.

Discuss your upgrade or trade-in

Aircraft-wing vibration questions

Explore the Q2 full-field measurement, optical geometry and engineering workflow demonstrated at ONERA.

What was measured on the MS.760 Paris aircraft?

At ONERA, Q2 measured the controlled vibration response of a Morane-Saulnier MS.760 Paris aircraft under nominal 10 Hz and 26 Hz excitation. The resulting full-field RMS velocity maps reveal how the observed structure responds across the measured area.

How was the vibration field captured?

Q2 acquired coherent line-of-sight velocity through 65 simultaneous optical channels at 40 kHz. Micro-scanning, repositioning and additional viewpoints extend the spatial map while preserving a common measurement workflow.

How does optical geometry support full-field analysis?

Each channel measures surface velocity along its line of sight. Beam-angle projection, geometric compensation and registered viewpoints connect those measurements to the aircraft geometry for operating-shape and modal analysis.

How does this workflow support aircraft dynamics programmes?

The non-contact maps support modal identification, structural-model correlation, test planning and fast comparison between excitation cases. Engineers can combine the optical field with reference sensors and programme acceptance criteria in a complete GVT workflow.

Explore the Q2 Laser RADAR