Satellite navigation system using multiple antennas

Data processing: vehicles – navigation – and relative location – Navigation – Employing position determining equipment

Reexamination Certificate

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C342S357490

Reexamination Certificate

active

07027918

ABSTRACT:
A satellite navigation system using multiple antennas for providing the position of multiple fiduciary points on an object even when fewer than four satellites are visible to some or all the antennas. Satellite signals from the multiple antennas are fed into at least one receiver. The receiver or receivers utilize constraint information, which is independent of the satellite signals. These external constraints are used to augment the signals received from the satellites, to obtain the position solution for each antenna. In a preferred embodiment, a common reference clock is used to provide an external constraint. Examples of other external constraints that can be used in the current invention are distance between the antennas, inertial measurement of attitude, rotational or linear position sensors, etc.

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“Maintaining GPS Positioning in Steep Turns Using Two Antennae,” by Lawrence, David G. et al.; Presented at the Institute of Navigation (ION) GPS-95; Palm Springs, CA; Sep. 1995; 9 pgs.

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