neoamorfic

AELIE™

neoamorfic™ · Atmospheric Entry / Launch Instability Engine

Deterministic structural instability diagnostics for ascent, hypersonic flight, and atmospheric entry using QEIv15™ invariants (entropy, curvature, φ-stress, λ-instability). Outputs a bounded instability index (IPI), a signed redline margin, and event markers. No learning. No prediction.

🚀 Partner Validation Required for Certification-Grade Use

AELIE™ is a deterministic structural instability indicator. It is not yet a certified flight-envelope authority. To reach certification-grade status, we seek partners able to provide: high-fidelity entry telemetry, known landmarks (max-Q, peak decel, blackout onset), and vehicle configuration metadata.

This enables calibration against ground truth and formal envelope validation.

License Key

Window

samples (rolling)

Upload Telemetry

Supported formats:
• GMN trajectory_points.txt (Time (s), Height (m), Vel (m/s))
• CSV (t/time, altitude/height, velocity/vel, optional acceleration)
• JSON telemetry (array or {telemetry:[...]})