Fixed wing
ALFA
UAV fault detection and anomaly detection
Fixed-wing fault benchmark with 47 autonomous segments, fault-onset/type labels, and supporting raw flight, telemetry and autopilot logs.
Access links
Primary places to inspect, download, read about, or reproduce the dataset.
Quick facts
- Vehicle type
- Fixed wing
- Environment
- Outdoor
- Data origin
- Real-world
- Sensor count
- 4
- Ground truth
- Available
- Calibration
- Not reported
- Annotations
- Available
Sensor overview
High-level sensor availability before the detailed sensor records below.
Ground truth
Reference scope, method, rate, coverage, and provenance.
| Scope | Method | Reference system | Count | Rate | Coverage |
Reference provenance
|
|---|---|---|---|---|---|---|
| Other | Other | Not reported | Not reported | 5 Hz | Partial · Processed Fault Scenarios |
Reference provenance
Derived
|
|
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Calibration and synchronization
Reported calibration level, reproducibility signals, and supporting notes.
- Level
- Not reported
- Processed parameters
- Not reported
- Raw calibration data
- Not reported
- Calibration targets
- Not reported
Calibration data
Calibration reproducibility details are not reported.
Notes
Not reportedKnown or intentional limitations
Reported constraints and characteristics to check before using the dataset.
47 processed cases include ten no-fault controls; the abstract wording does not establish 47 faulty flights.
Fault-onset topics can lag the injected event by up to 0.2 seconds.
Fault truth is absent from raw telemetry/dataflash collections and does not establish independent pose truth.
Sudden recoverable faults dominate; gradual and sensor faults are outside this release.
Measured airspeed is nonzero in 13 of the 47 processed sequences; 34 have zero-filled channels. The paper reports a 20–25 Hz commanded/measured topic rate; native sampling and a consistent recorded cadence are unverified. Commanded airspeed is a controller target. Probe model, airspeed convention and released differential pressure are unreported.
Cameras
IMUs
Pixhawk dataflash inertial units
- Model
- Not reported
- Count
- 2
- Accel / gyro
- Not reported
GNSS
Onboard GPS
- Model or name
- Onboard GPS
- Count
- 1
- Rate
- Not reported
- GNSS type
- NOT REPORTED
- Position output
- Available
- Velocity output
- Not reported
- Heading output
- Not reported
LiDAR
Radar
Pitot tube
Pitot airspeed measurements
- Model or name
- Pitot airspeed measurements
- Count
- 1
- Rate
- Not reported
- Airspeed output
- Available
- Differential pressure
- Not reported
- Notes
- Measured airspeed is nonzero in 13 of the 47 processed sequences; 34 have zero-filled channels. The paper reports a 20–25 Hz commanded/measured topic rate; native sampling and a consistent recorded cadence are unverified. Commanded airspeed is a controller target. Probe model, airspeed convention and released differential pressure are unreported.
Additional sensors
Annotations
Reported annotation availability and task support.
- Availability
- Available
- Format
- ROS fault-status topics; CSV; MAT
- Class count
- Not reported
Citation
Citation key and BibTeX kept at the end of the page for reference.
@article{keipour2021alfa,
title = {ALFA: A Dataset for UAV Fault and Anomaly Detection},
author = {Keipour, Azarakhsh and Mousaei, Mohammadreza and Scherer, Sebastian},
year = {2021},
journal = {The International Journal of Robotics Research},
volume = {40},
number = {2-3},
pages = {515--520},
doi = {10.1177/0278364920966642},
}
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