Method for reducing in-transit navigational errors
A method for improving the accuracy of an inertial navigation system (INS) by performing a synchronization procedure to align the INS to a compass-derived initial heading comprises the steps of determining a heading of minimal error for the compass and defining that heading as the initial heading; orienting the INS to align with the so-defined initial heading; synchronizing the internal navigation system to that heading; and proceeding with navigation by use of the INS. The INS may be vehicle mounted or be contained in a portable navigation unit for swimmers or other users. The heading of minimal error may be determined by placing the compass within a multi-axis Helmholz coil system and monitoring compass readings and deviation errors as a function of actual compass positions.
1. A method for improving the accuracy of an inertial navigation system (INS) by performing a synchronization procedure to align the INS to a compass-derived initial heading utilizing a previously prepared display of compass error as a function of indicated heading over a 360 degree circumference, comprising the steps of:
a. utilizing the display of compass error to determine a heading of minimal error for the compass and defining that heading as the initial heading;
b. orienting the INS to align with the so-defined initial heading;
c. synchronizing the internal navigation system to that heading; and
d. proceeding with navigation by use of the INS.
2. The method of claim 1 wherein the INS is associated with a vehicle.
3. The method of claim 1 wherein the display of compass error is formed by placing the compass within a multi-axis Helmholz coil system and monitoring the compass reading as a function of actual compass positions with respect to a known orientation of the magnetic field generated by the coil system and obtaining deviation values for various compass positions.