Validation and development status
What is measured today, what is calculated, and what remains open. This page deliberately states the limits too – they matter more for assessing the project than the most flattering numbers.
The currently permitted claim
The frozen V1 path produces a motion and track candidate. The permitted statement is possible moving drone candidate – not confirmed drone. A productive person-versus-drone decision, an angle or spatial-identity claim, or an alert derived from the candidate label alone are not permitted without new evidence.
Radar range figures routinely conflate three entirely different quantities into a single "range". At Ozense they are kept explicitly apart:
| Quantity | Value | What it means |
|---|---|---|
| Sampling/evaluation boundary | about 30 m | A configuration choice of the current waveform, which is optimised for high range resolution – not a property of the sensor and not a detection guarantee. |
| Instrumented boundary | about 28.7 m | Follows from the edge window of the current CFAR detector. Beyond it, nothing is evaluated at all. |
| Credible field tracking | so far around 14–20 m | The result actually measured on small drones in field data to date. This is the only demonstrated figure. |
The gap between 30 m and 14–20 m is not a contradiction but the usual distance between a detection boundary without margin and a track range. A modelled range only becomes a track range once probability of detection, track promotion and track retention have been measured statistically against distance.
A link budget can compute an SNR-limited range from transmit power, antenna gain, bandwidth, integration time and noise figure. For the hardware in use, that calculation shows a physically plausible path to greater distances – under assumptions that have not yet been measured together.
Binding rule of language: range is a problem of aperture, dwell and integration, not a chip problem. But any figure in metres is worthless without stating target radar cross section, detection threshold and integration time. Datasheet ranges for automotive sensors refer to vehicle targets and must not be transferred to drones; the difference in backscatter is 25 to 35 dB, a range factor of roughly 4 to 6.
Specifically open:
- Whether the integration needed for longer observation times remains usable coherently, or fails on range and Doppler migration.
- Whether the assumed individual gains from coherent beamforming, longer dwell and track-before-detect actually behave additively – they have not been measured together.
- That longer observation times conflict directly with alert latency: a target at 15 m/s covers about 24 m in 1.6 s.
- That rain, a wet radome, radome insertion loss and enclosure and mounting effects on antenna pattern and phase are not yet quantified. Until then, all range forecasts are fair-weather laboratory assumptions.
- That flight elevation is a highly sensitive parameter: at 1.5 m radar height and 14 m range, an altitude of 5 m already costs about 5.8 dB two-way – and it was not recorded in any field session so far.
It follows that greater ranges are development forecasts, not product properties. No fixed product range is claimed.
A result is worth only as much as the procedure that produced it. Ozense therefore works with a pre-registered evaluation chain:
- Pre-registration. Thresholds and evaluation logic are fixed before the evaluation data is inspected. A gate is not readjusted after an independent holdout has been seen.
- Data separation. Development, validation and independent holdout data are kept strictly apart.
- Reproducibility. Raw replay and evaluation are version- and hash-bound, so a result can be regenerated from the same raw data.
- External ground truth. Target positions are checked against an independent reference, not against the system's own processing chain.
- Stage-wise evaluation. Detector, tracker, track validity and semantic assessment are reported separately rather than netted into one end metric.
This discipline is uncomfortable: it has repeatedly forced earlier internal results to be discarded as unsound. That is precisely its purpose.
| Building block | Status | Limit of the statement |
|---|---|---|
| Radar capture and evaluation | Working | Short range; not a long-range radar |
| Detection and tracking | Working | Moving candidates with sustained Doppler evidence |
| Evaluation chain / reproducibility | Pre-registered and sealed | A parity result, not a performance result |
| Independent field holdout | Outstanding | Without it no acceptance result is possible |
| Drone/bird/clutter in the field | Not robustly demonstrated | Synthetic results show modelling capability, not field performance |
| Sim-to-real transfer | Domain shift visible | Recalibration and shift detection are funding-phase goals |
| Angle of arrival | Not released productively | Angle-dependent features stay disabled until board calibration |
| PTZ cueing and VMS end-to-end | Not demonstrated | Camera ground-truth tooling exists; the product function does not |
| Weather and site robustness | To be validated | Rain, radome and mounting losses not quantified |
| Series hardware and product release | Not available | No released, populated series board |
- No confirmed drone identity. The output is a candidate, not a determination.
- No fixed product range. 14–20 m of field tracking is demonstrated; everything beyond that is calculated.
- No guaranteed field false-alarm rate. Uncertainty-calibration methods hold only under their own assumptions, and under domain shift those assumptions no longer apply.
- No blanket GDPR compliance. Local, event-driven processing eases the data protection assessment but does not replace it.
- No KRITIS certification, and no claim that operators are legally obliged to deploy a drone radar.
- No automatic frequency permission. Fixed-site operation in the 76–81 GHz band requires separate clearance; an application for research use is pending with the German Federal Network Agency.
- Not a counter-drone effector. Ozense detects, assesses, documents and alerts. No neutralisation.
Absolute SNR calibration
Measurement against a trihedral reflector of known radar cross section, with identical azimuth and elevation geometry for reflector and drone. The goal is an exact rather than merely plausible match between model and field.
Independent field holdout
A pre-registered campaign with drone, person and clutter runs plus mandatory empty scenes – with no retrospective tuning against the results.
Bird ground truth
Because bird discrimination is part of the claim, it needs a reproducible reference procedure: a synchronised optical reference with multi-stage adjudication; ambiguous cases are excluded rather than force-labelled.
Quantify external losses
Rain, wet radome, radome insertion loss and enclosure and mounting effects on antenna pattern and phase are tracked as their own measurement items.
Looking for measurement partners and pilot sites.
Particularly valuable: an independent measurement partner for range calibration, and areas where measurements may be taken under real clutter conditions.
Discuss a pilot partnership