Local Level Lab

Airborne measurements. Open methods.

Compare the raw pitch trend with geographic predictions

The raw gyroscope plot shows accumulated pitch-axis increments without a fitted calibration or GPS subtraction. Its companion will ask a different question: does the variation between recordings follow predictions made from their course, speed and latitude?

An IMU (inertial measurement unit) measures turning with gyroscopes and specific force with accelerometers. Here the recorded gyro increments remain the turning observations. Receiver positions supply the trajectory context for the predictions; they do not supply a replacement gyro signal.

A transparent reference prediction

For a level aircraft whose nose follows its ground course, the globe transport contribution around its right-pointing axis is approximately -speed/radius. The specified background field adds -Omega*cos(latitude)*sin(course). The flat candidate's transport is a vertical yaw contribution, with no pitch component under these level-flight assumptions. The exact companion will retain the declared candidate metrics, rather than use this approximation silently.

This calculation must show its assumptions. Aircraft heading can differ from ground course, roll and pitch can project yaw onto the recorded pitch axis, and genuine aircraft pitching remains in the raw sum. A sensitivity envelope may vary declared attitude/crab assumptions, but cannot call them measured. Possible upstream field removal is shown separately and equally for candidates.

Planned output and controls

Freeze generated controls, data identities and a finite allowance before execution. No new physical-model fits are needed. This diagnostic does not replace withheld prediction, uncertainty assessment or the planned free-field measurement.

Study index · Roadmap · Free rotation-field study.