Abstract: | Honeywell and its teammates, Allied Signal and Trim- ble, have developed a design for a compact (100 it?) integrated Global Positioning System/Inertial Navigation System (GPWINS) under the GPS Guidance Package (GGP) Program funded by DARPA. This effort included developing new inertial sensor technology and imple- menting inertial aiding of the GPS receiver’s tracking loops. The inertial sensors consist of fiber-optic gyro- scopes and solid-state silicon accelerometers suitable for a I-nmi/hr-class navigation system. Inertial aiding of the GPS receiver’s carrier tracking loop was used to enhance tracking under severe dynamics without compromising anti-jam performance. This paper reviews the hardware and software architec- ture, packaging approach, and test results from a proto- type unit. These tests demonstrated the capabilities of the overall system, including integrated GPS/INS navi- gation and enhanced performance of the GPS receiver as a result of carrier loop aiding. |
Published in: |
Proceedings of the 53rd Annual Meeting of The Institute of Navigation (1997) June 30 - 2, 1997 Albuquerque, NM |
Pages: | 639 - 648 |
Cite this article: | Bye, Charles T., Hartmann, Gary L., Killen, Albert, "Inertial and GPS Technology Advances on the GGP Program," Proceedings of the 53rd Annual Meeting of The Institute of Navigation (1997), Albuquerque, NM, June 1997, pp. 639-648. |
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