Inertial navigation

The Schuler period is 2π√(R/g). R is the GRS80 mean radius, …, and g is the stated standard gravity. An uncorrected accelerometer bias walks the position. The curve is that walk. Earth-rate compensation depends on latitude the same way as the Foucault page: the sidereal rate times the sine of the latitude. This page has no waypoints, and it does not claim to align a real system.

The bias 0.001 m/s² is an example. It is not a measured instrument. Stockholm is 59.3293° N. Sydney is 33.8688° S. Both are the city positions already used on this site.

The curve is ½ b t² for two hours. It is the open-loop walk, not a Schuler oscillation and not a flight.

  • Position error
  • The value at two hours

Schuler period

2π√(R/g)
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Uncorrected bias

Position after one hour
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Earth rate

sin(latitude)
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What this page shows

A pendulum as long as the Earth’s radius, or an inertial navigator tuned the same way, has the period 2π√(R/g). The card is that period. R is the shared mean radius. g is 9.80665 m/s², the conventional standard gravity, not a gravity measured at the latitude you type.

Without that tuning, a constant accelerometer bias b is integrated twice. The position error is ½ b t². The curve is that parabola for two hours, and the card is the error after one hour. A negative bias walks the other way. This is not a flight path.

Compensating for the Earth’s rotation depends on latitude the same way as the Foucault page. The vertical component is the sidereal rate times sin(latitude). North of the equator the sense is clockwise, as on that page. South of the equator it is anticlockwise. At the equator there is none of that rate. The sidereal day is the one the Foucault page uses. Saying so is not a claim that the page aligns a real system.

Assumptions

Sources