Requirements.StabilityRequirement

SR-WIND-02: The UAS shall maintain lateral and yaw stability under wind disturbance and recover within limits

Information

SR-WIND-02 – Performance in Wind

Source: EASA Means of Compliance Light-UAS.2512, ISO 21384-3 (Clause 10 – Operational limitations).

Requirement:
Under a steady 8 m/s wind with 12 m/s gusts, the UAS shall:

• Maintain lateral position error ≤ 1.5 m (95th percentile) during hover.
• Maintain yaw pointing error ≤ 5° (95th percentile).
• Recover to within 0.5 m acceptance enveloppe position error within 3 s after gust disturbance.

Simulation Inputs: Connect to AIDA_System position, yaw, and reference signals.

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