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id
stringclasses
6 values
flight_phase
stringclasses
6 values
aircraft_context
stringclasses
6 values
engine_params_summary
stringclasses
6 values
aero_state_summary
stringclasses
6 values
control_surface_summary
stringclasses
6 values
coupling_coherence_index
float64
0.63
0.86
baseline_correlation_matrix
stringclasses
6 values
phase_alignment_score
float64
0.58
0.82
stability_envelope
stringclasses
6 values
lag_profile
stringclasses
6 values
baseline_confidence
float64
0.64
0.84
notes
stringclasses
6 values
constraints
stringclasses
1 value
gold_checklist
stringclasses
1 value
PACB-001
cruise
A320; ISA; stable mass
N1 86-88; EGT 610-630; FF 2400-2550
IAS 280-285; ALT FL350; AoA 2.2-2.6
elevator small; aileron small; trim stable
0.86
N1-IAS:0.78|N1-AoA:-0.52|FF-IAS:0.74|EGT-IAS:0.41
0.82
0.78-0.92
engine->IAS 1.5s; engine->AoA 1.8s
0.84
High coherence cruise baseline
Under 260 words
idx+corr+phase+env+lag+conf
PACB-002
climb
A320; ISA+5; heavy
N1 92-96; EGT 680-720; FF 3100-3600
IAS 250-265; ALT 9000-17000; AoA 4.0-5.2
elevator active; trim moving
0.74
N1-IAS:0.62|N1-AoA:-0.46|FF-ALT:0.71|EGT-ALT:0.38
0.7
0.62-0.82
engine->IAS 1.8s; engine->ALT 2.6s
0.76
Climb has wider envelope
Under 260 words
idx+corr+phase+env+lag+conf
PACB-003
takeoff roll
A320; dry; normal
N1 96-99; EGT 720-760; FF 4200-4600
IAS 0-155; ALT 0; AoA 0-3
rudder active; spoilers retracted
0.8
N1-IAS:0.86|FF-IAS:0.82|EGT-IAS:0.54|N1-AoA:-0.22
0.78
0.70-0.88
engine->IAS 0.8s; engine->AoA 1.1s
0.79
High direct coupling on roll
Under 260 words
idx+corr+phase+env+lag+conf
PACB-004
approach
A320; gusty; landing conf
N1 52-68; EGT 480-560; FF 1400-2100
IAS 135-155; ALT 3000-500; AoA 6.5-9.0
flaps extended; spoilers armed; elevator active
0.66
N1-IAS:0.55|N1-AoA:-0.40|FF-IAS:0.52|EGT-IAS:0.30
0.62
0.52-0.76
engine->IAS 2.2s; engine->AoA 2.6s
0.68
Gusts reduce coherence
Under 260 words
idx+corr+phase+env+lag+conf
PACB-005
descent
A320; smooth; idle segments
N1 28-45; EGT 380-460; FF 900-1300
IAS 260-290; ALT FL330-FL180; AoA 1.5-3.0
speedbrake intermittent; trim stable
0.71
N1-IAS:0.44|FF-IAS:0.48|N1-ALT:0.36|EGT-IAS:0.22
0.6
0.58-0.80
engine->IAS 2.8s; engine->ALT 3.2s
0.66
Idle reduces coupling strength
Under 260 words
idx+corr+phase+env+lag+conf
PACB-006
holding
A320; moderate turbulence
N1 58-66; EGT 500-560; FF 1600-2000
IAS 210-230; ALT 12000; AoA 4.8-6.2
bank changes; elevator active
0.63
N1-IAS:0.50|N1-AoA:-0.34|FF-IAS:0.46|EGT-IAS:0.26
0.58
0.48-0.74
engine->IAS 2.0s; engine->AoA 2.4s
0.64
Turbulence widens envelope
Under 260 words
idx+corr+phase+env+lag+conf

What this dataset tests

Whether a system can model the normal coupling between propulsion parameters and aerodynamic state.

The signal is relationship shape and lag not threshold breaches.

Required outputs

  • coupling_coherence_index
  • baseline_correlation_matrix
  • phase_alignment_score
  • stability_envelope
  • lag_profile
  • baseline_confidence

Scoring conventions

  • all scores range 0 to 1
  • stability envelope is a low-high interval
  • lag profile describes expected response delays in seconds
  • correlation matrix is a compact cross-system summary

Use case

Layer one of Propulsion–Aerodynamics Coupling Decoherence Signatures.

Supports:

  • precursor detection via coupling drift
  • early warning before engine alarms
  • context-aware stability envelopes by flight phase
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