Method of increasing location accuracy in an inertial...

Details Method of increasing location accuracy in an inertial... Method of increasing location accuracy in an inertial...

2002-02-19

2003-09-02

Marc-Coleman, Marthe Y. (Department: 3661)

Data processing: vehicles, navigation, and relative location

Navigation

Employing position determining equipment

C701S208000, C340S995190

Reexamination Certificate

active

06615136

ABSTRACT:

FIELD OF THE INVENTION
The present invention relates generally to a method if increase location accuracy in an inertial navigation device.
BACKGROUND OF THE INVENTION
A traditional inertial navigation system (“INS”) in its embodiment utilizes accelerometers, gyroscopes, and support electronics, such as a processor, in order to translate sensor data into motional changes. These changes are then translated to position based on an initial referenced position and the integration or differentiation of said motion. As time progresses, the errors associated with the accelerometers and gyroscopes increase to a point where the translation to position is outside of the required positional resolution, thus rendering the unit ineffective or lost.
In one INS embodiment, the INS device is updated manually by resetting the INS device using a known fixed position or by returning back to the original reference position. The user manually resets the INS unit and positional errors are cleared until said error occurs again requiring another reset.
In another embodiment the INS device is updating an alternate location-finding unit, such as a global positioning system (“GPS”). In this configuration, the attached GPS is providing data to a communication link sending back Latitude and Longitude information. The INS device is utilized when the GPS position is no longer available due to occulting of the satellites. The INS device is utilized to provide updates to the last known position and errors are accumulated at a rate of 2% to 5% of the distance traveled. The INS device is only used for updating the embedded GPS unit's location. Once a GPS signal is re-captured, the INS device is not used.
Traditionally, INS devices utilize output voltages representing the second derivative of position to integrate and determine relative changes in motion. These are applied to the last known position update and a new one is generated with some small error. As time progresses, the errors are accumulated and the computed position is no longer usable by the INS user. A known location or position is required in order to correct for the errors. Traditional systems utilize GPS, or cycle through a fixed reference point to correct those errors.
Thus, there exists a need for a system that reduces error accumulation and performs stand-alone tracking in areas where GPS (or other similar location technologies) can no longer provide location updates to the user or infrastructure.


REFERENCES:
patent: 5781156 (1998-07-01), Krasner
patent: 2002/0062193 (2002-05-01), Lin
patent: 2002/0116125 (2002-08-01), Lin

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