Datasets:

ClarusC64
/

aviation-pilot-vehicle-loop-coherence-state-estimation-v0.1

id stringclasses 6 values	aircraft_context stringclasses 1 value	flight_phase stringclasses 6 values	abnormal_condition stringclasses 6 values	control_input_summary stringclasses 6 values	aircraft_response_summary stringclasses 6 values	coupling_features stringclasses 6 values	loop_coherence_index float64 0.44 0.92	resonance_stability_band stringclasses 3 values	control_lag_profile stringclasses 6 values	correction_efficiency_score float64 0.41 0.93	baseline_deviation float64 0.06 0.48	notes stringclasses 6 values	constraints stringclasses 1 value	gold_checklist stringclasses 1 value
LCE-001	A320	go-around	flap asymmetry	rapid pitch inputs; thrust surge	delayed pitch response; roll bias	lag 0.9s; asymmetric coupling	0.44	unstable	lag high 0.9s	0.41	0.48	pilot fighting aircraft	Under 240 words	idx+band+lag+eff+dev
LCE-002	A320	final approach	none	smooth pitch corrections	expected response	lag 0.2s; symmetric	0.92	stable	lag low 0.2s	0.93	0.06	healthy loop	Under 240 words	idx+band+lag+eff+dev
LCE-003	A320	climb	engine surge	abrupt throttle corrections	oscillatory thrust response	lag 1.1s; thrust mismatch	0.51	unstable	lag high 1.1s	0.47	0.42	aircraft-driven mismatch	Under 240 words	idx+band+lag+eff+dev
LCE-004	A320	descent	pilot startle	overcorrection roll	stable aircraft	lag 0.3s; pilot amplitude high	0.58	fragile	lag moderate	0.52	0.33	pilot overcontrol	Under 240 words	idx+band+lag+eff+dev
LCE-005	A320	takeoff	sensor disagreement	trim oscillation	inconsistent pitch response	lag 0.7s	0.49	unstable	lag 0.7s	0.46	0.39	sensor-driven	Under 240 words	idx+band+lag+eff+dev
LCE-006	A320	holding	turbulence	minor corrections	expected turbulence response	lag 0.4s	0.78	stable	lag 0.4s	0.76	0.19	environment only	Under 240 words	idx+band+lag+eff+dev

What this dataset tests

Whether a system can estimate the coherence
of the pilot–aircraft control loop
during abnormal phases.

Key insight
Loss of control begins
with loop misalignment
before any hard limits are exceeded.

Required outputs

loop_coherence_index
resonance_stability_band
control_lag_profile
correction_efficiency_score
baseline_deviation

Use case

Layer one of Pilot–Vehicle Loop Coherence Under Stress.
Feeds attribution and adaptive intervention systems.

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