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GoFast Case Resolution

All-domain Anomaly Resolution Office · 26 pages · text from the file's own layer

The All-domain Anomaly Resolution Office of the U.S. Department of Defense issued this case resolution on the "Go Fast" video on February 6, 2025. It covers a January 2015 FLIR recording made by a U.S. Navy F/A-18F off Florida's eastern coast. From the public 34-second video, AARO puts the object at about 13,000 feet, moving at 5 to 92 mph relative to the wind. It attributes the apparent high speed to motion parallax and has high confidence the object showed no anomalous performance.

  • p. 8 …The angle of rotation about the x-axis is the aircraft roll and is denoted by…
  • p. 9 UNCLASSIFIED 9 UNCLASSIFIED elevation and denoted by β; the angle of rotation about the z-axis…
  • p. 10 …This rotation away from the axis can be represented as a yaw angle of φ relative…
  • p. 11 …The additional yaw of the F/A-18 of -9.6° required one additional rotation.5…
  • p. 12 …0 (9𝑎) = 5158 0 3612 (9𝑏) The rotation about the z-axis by -57° to account…
  • p. 15 …With values estimated for all frames and times, the vector rotation and point translation methodology described…
  • p. 26 …more details on matrix multiplication and angle rotations about the cartesian axes. 7. Refer to Section…
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Determining the object’s true speed and direction of travel (heading) requires knowing the F/A-
18F’s heading. AARO calculated the object’s speed and heading relative to the aircraft because
the video display does not contain the aircraft’s heading. AARO calculated the object’s position
and direction of travel for the entire range of possible wind directions (0° - 360°) to account for
differences in atmospheric conditions between the F/A-18F’s altitude and object’s altitude. This
comprehensive modeling informed AARO’s assessment of whether the object moved with or
against the wind and whether it behaved anomalously for all possible directions of travel.
AARO factored in historical wind speeds and directions at both the object’s altitude (13,000 feet)
and the aircraft’s altitude (25,000 feet), as measured near the time and location of the event:
• At 13,000 feet, wind speed was 30.9 m/s (69 mph) from the west (265°).
• At 25,000 feet, wind speed was 52 m/s (116 mph) from the west southwest (255°).
Figure 1 shows the object’s range of possible speeds calculated while compensating for wind
speed at 13,000 feet. This is considered the “intrinsic” speed. An intrinsic speed of 0 m/s
indicates that the object is moving with the wind, or about 30.9 m/s.
Figure 1: The y-axis represents the object’s speed with wind effects removed. The x-axis represents the wind’s
heading relative to the F/A-18F’s airframe geometry (0° is a headwind). The curve represents the object’s range of
speeds at each angle. The tailwind, headwind, and crosswind cases are denoted by the colored lines. The object’s
lowest possible speed occurs near a headwind while the highest occurs in a tailwind.
Figure 2 shows the object’s range of possible headings relative to the wind direction at 13,000
feet A direction of 0° indicates that the object is moving in the same direction as the wind.

Cases discussed

About this file

Analysis, from the aaro collection. The PDF is mirrored here; the original link is under it. 26 pages are in the text index: search them above, or from the library's search.