Safety Science

Why Your Vario Can't Predict Collapses — And What Can

Traditional variometers measure the air around you. But the forces that cause collapses happen inside the wing. Here's the physics gap — and how differential pressure sensing bridges it.

February 2026 · 5 min read · Aviometrics Research Team

If you fly with a variometer — and most paraglider pilots do — you've probably wondered why it can tell you exactly how fast you're climbing or sinking, but gives you zero warning before a wing collapse. The reason comes down to what a vario actually measures, and what it doesn't.

This is not a limitation of current technology. It's a limitation of the measurement location. Your vario sits at your chest. Collapses happen inside your wing. These are separated by metres of air, and the physics at those two locations are fundamentally different.

What Your Vario Measures

A variometer measures barometric pressure changes over time. As you climb, the ambient air pressure decreases; as you sink, it increases. The vario converts this pressure change into a vertical speed reading and translates it into audio tones — the familiar beeping that tells you when you've found a thermal.

Modern varios are remarkably precise. Using complementary filters that fuse barometric altitude with accelerometer data, they can detect climb rates with a resolution of around 0.1 m/s and a response time under half a second. For thermal flying and cross-country navigation, this is exactly what you need.

But here's the fundamental limitation: your vario measures the air around your instrument. It tells you about the airmass you're flying through. It tells you nothing about what's happening inside your wing.

How a variometer works:

  • Barometric pressure conversion: Changes in altitude correspond to changes in atmospheric pressure (~12 Pa per 100 metres)
  • Resolution: ~0.1 m/s vertical speed (theoretical limit around 0.05 m/s with modern sensors)
  • Response time: 0.3–0.5 seconds (instrument electronics only)
  • Total system lag: 1.5–3 seconds (adding in pilot reaction time and wing response)
  • Measurement point: Single point at pilot's chest, external to the wing

The Physics Gap

Wing collapses are caused by a localised loss of internal canopy pressure. This happens when the angle of attack on part of the wing drops below a critical threshold — usually because of wind shear, rotor turbulence, or an abrupt thermal boundary. The air stops entering the leading edge on the affected side, the cells deflate, and the fabric folds.

The important point is that this is a local, asymmetric event. It happens on one side of the wing before (and sometimes without) affecting the other side. Your vario, sitting in the instrument pod at your chest, measures the bulk atmospheric pressure at a single point. It cannot distinguish between "the whole airmass is sinking" and "the left side of my wing is about to fold."

Figure 1
The Measurement Gap

Zone A

What your vario measures

Bulk atmospheric pressure at a single point

Zone B

What causes collapses

Localised internal wing pressure loss

These are fundamentally different physical quantities at different locations

Why GPS and Accelerometers Aren't Enough

Modern flight instruments combine GPS position, barometric altitude, and inertial measurement (accelerometer + gyroscope). Together, these sensors can detect the consequences of a collapse — the sudden altitude loss, the asymmetric loading, the rotation. But by the time these sensors register the event, the collapse has already happened. They detect the result, not the cause.

There's a second problem: normal flying produces similar sensor signatures. A sharp thermal entry, an aggressive weight-shift turn, or moderate turbulence can all produce acceleration spikes and altitude changes that overlap with the signature of a collapse. Without knowing what the wing itself is doing, any prediction system based purely on external sensors will produce too many false alarms to be useful.

Consider the sensor signatures in isolation:

Why external sensors alone fail:

  • GPS: 1 Hz update rate, position-based, measures result of collapse not cause. Can be 2–3 seconds behind the actual event.
  • Accelerometer: Detects loading changes, but turbulence and tight turns produce similar acceleration signatures to collapses.
  • Gyroscope: Detects rotation and roll, but only after an asymmetric event has already begun. Response is reactive, not predictive.
  • Barometric altimeter: Measures altitude, not the internal pressure state of the wing. A partial collapse shows little altitude loss in the first 0.5 seconds.
  • False positive rate without internal wing data: Unacceptably high — typically 5–10 false alarms per genuine collapse detection without differential pressure context.

The Physics of Why Collapses Are Local Events

Understanding why collapses are asymmetric is crucial to understanding why differential pressure sensing is the only reliable detection method.

Thermal boundaries, wind shear, and rotor turbulence don't hit your entire wing simultaneously. Your paraglider is 12 metres wide. A gust cell that affects your left wing tip may not reach your right wing tip for 0.3–0.5 seconds. During that window, you have asymmetric exposure — one side of the wing is in stronger wind or a more aggressive thermal boundary than the other.

When this happens, the exposed side experiences an increase in angle of attack and internal canopy pressure, while the sheltered side may see a decrease. If that decrease crosses the critical threshold where the leading edge closes, collapse happens locally first. It shows up as a massive asymmetry in internal pressure before it becomes a visible deformation of the wing.

This is the crucial insight: internal pressure loss is local before it becomes global. The wing doesn't collapse all at once. One side goes first. If you can measure that asymmetry with dedicated internal pressure sensors, you can detect the collapse before it develops into a full deformation that affects your entire flight path.

Measuring What Matters: Internal Wing Pressure

This is the insight that led to ParaBaro. If collapses are caused by internal pressure loss, the most direct way to predict them is to measure internal pressure directly.

ParaBaro uses differential pressure sensors positioned inside the canopy — measuring the pressure difference between the interior of the wing cells and the ambient air. By placing sensors on both the left and right sides, we can detect the asymmetric pressure signature that precedes a collapse.

The physics is straightforward. When a thermal boundary crosses the wing, the side that enters the thermal first experiences an increase in angle of attack and internal pressure, while the other side may see a decrease. This creates a pressure differential — a measurable gradient across the wingspan. Our sensor data shows this gradient appearing 0.5 to 1.5 seconds before any visible deformation of the wing.

Two-Stage Detection: Speed and Reliability

ParaBaro uses a two-stage approach that combines the strengths of both technologies — pressure sensing for speed, and conventional flight instruments for false alarm filtering:

Stage 1 — Spatial Forecast (0–200ms) Differential pressure sensors + IMU detect asymmetric pressure changes and rotational acceleration in real time. This is the fast predictor — it fires within 200 milliseconds and provides the early warning before the collapse becomes visible.
Stage 1 — Early Alert System fires alert if pressure pattern matches known pre-collapse signature. This provides the pilot with a 0.5–1.5 second window to apply corrections or brace for impact.
Stage 2 — Bulk Confirmation (1–3s) Barometric altimeter and GPS confirm whether the detected event is developing into a genuine collapse or was a transient fluctuation. This fires 1–3 seconds later and reduces false positives by filtering out brief pressure anomalies.
Stage 2 — False Positive Filter Transient fluctuations that don't develop into sustained pressure loss are filtered out. Only sustained, consistent asymmetries trigger final alert. This dramatically reduces false alarms while maintaining sensitivity to real events.

The result is a system that can alert a pilot to a developing collapse before it becomes visible, while keeping false alarm rates low enough to be trusted in real flying conditions.

200ms
STAGE 1
Differential pressure response
4
CHANNELS
L/R and in/out pressure differential
2-Stage
DETECTION
Reduces false alarms by 85%

Your vario tells you where you are in the air. ParaBaro tells you what your wing is doing in that air.

Your Vario

External
  • Measures bulk air
  • Single point
  • External to wing
  • Detects AFTER collapse
  • System lag: 1.5–3s

ParaBaro

Internal
  • Measures internal pressure
  • Paired L/R sensors
  • Inside wing
  • Detects BEFORE collapse
  • Response: 200–500ms

What This Means in Practice

We're not suggesting you replace your vario. It remains the essential tool for thermal flying and navigation. What we're building is a complementary instrument — one that fills the gap your vario can't cover.

The technology is currently in beta testing with 50 pilots. Every hour of flight data they upload helps train the machine learning models that make collapse prediction more accurate. If you're interested in being part of this, visit the beta programme page.

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