Abstract: An apparatus comprising a position system configured to determine a global positioning (GPS) change vector, and an inertial navigation system (INS) change vector. The position system is configured to determine a relative position between a first platform and a second platform based on the GPS change vector and the INS change vector, and the position system is configured to correct a GPS position calculation error based on the GPS change vector and the INS change vector.
Type:
Grant
Filed:
May 20, 2009
Date of Patent:
May 1, 2012
Assignee:
Northrop Grumman Guidance and Electronics Company, Inc.