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Inertial navigation is the art of knowing where you are without asking anyone. An Inertial Measurement Unit (IMU) — three gyroscopes and three accelerometers — measures angular rate and specific force. By integrating these measurements over time, an Inertial Navigation System (INS) computes attitude, velocity and position entirely on its own: no satellites, no radio beacons, no external references.
That self-reliance is exactly why inertial navigation matters more than ever. GNSS signals are weak, easily jammed and increasingly spoofed. In a contested environment, your IMU is the one sensor that cannot be denied.

The strength of inertial navigation — integration — is also its weakness. Every sensor error, however small, is integrated right along with the signal. Navigation errors don't stay constant; they grow.
| Error source | Position error growth | What it means |
|---|---|---|
| Gyroscope bias | ∝ t³ | Tilts the attitude estimate, misprojects gravity, then integrates twice more — dominates INS grade. |
| Accelerometer bias | ½·b·t² | A 1 mg bias means ~18 m of position error after just 60 seconds. |
| ARW / VRW (noise) | ∝ √t | Sets the floor on performance even with perfect calibration. |
| Bias instability | slow wander | How far the bias drifts over minutes and hours — the limit of what estimation can remove. |
| Scale factor & misalignment | scales with dynamics | The harder you maneuver, the more they hurt. |
The takeaway: an unaided INS is a clock that is always running down. The question is never whether errors grow — it's how fast, and whether that rate is acceptable for your mission duration and accuracy requirement.
Datasheets are full of numbers; only a few of them decide whether your system works.
These two numbers determine free-inertial drift more than any others. Consumer MEMS: tens of °/h. Tactical: 0.5–10 °/h. Navigation grade: below 0.01 °/h. Match the grade to your GNSS-denied endurance — not to the best case.
Critical for velocity accuracy and alignment: a 1 mg bias limits initial leveling to ~1 mrad of tilt error.
Bias over the full temperature range, turn-on repeatability, vibration rectification (VRE) and shock survivability matter more in the field than headline noise figures.
High-dynamic platforms need enough sensor bandwidth to capture the motion, and deterministic low-latency output for the control loop.
The best IMU is the lightest, cheapest one that still meets your drift budget — with margin.
No IMU flies alone forever. How gracefully the fusion degrades when GNSS, odometry or other aiding disappears is a system-level property worth evaluating as carefully as the sensor.
Two IMUs built from the same sensors can perform worlds apart — the difference is calibration. At ATEŞ Labs, every aSense unit goes through a custom in-house calibration procedure covering the full operational temperature range, not just room temperature:
A datasheet quotes numbers; calibration is what makes a unit meet them on a vibrating airframe at −40 °C.
We design and build the aSense family of tactical-grade IMUs and GNSS/INS systems for resilient navigation in GNSS-denied environments. If you're sizing an inertial solution for your platform, we'd be glad to help you work through the error budget and find the right fit.
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