GPS Orion Receiver Development Page

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The GPS Orion receiver is a sample receiver design provided by Mitel Semiconductor (now Zarlink). It serves as a prototype for industrial GPS receivers built around the Mitel GP2000 chipset and is supplemented by the GPS Architect Software Development Kit (no longer supported).

Last update: 18-OCT-2002
Created: 26-JUN-2002
Contact: Takuji Ebinuma

Firmware Modifications

For use on low Earth orbit satellites and other space applications, numerous software modifications and enhancements have been made to the original firmware of the Orion receiver. These modifications include the fixes related to the implicit assumption of a low speed vehicle in the Doppler prediction and the time tagging error of the raw measurements. Aside from these fixes, an open-loop Doppler and visibility prediction algorithm has been added to the receiver code to ensure a robust tracking and rapid signal acquisition under the conditions of a high-dynamic space vehicle. Also, an active alignment of measurement epochs and navigation solutions to the integer second of GPS system time has been implemented, which ensures synchronized measurements among multiple independent receivers. To improve the overall navigation performance of the Orion receiver, integrated carrier phase measurements have been made available using a 3rd order phase lock loop (PLL) assisted by a 2nd order frequency lock loop (FLL). The loop provides accurate tracking and stable acquisition over a wide range of dynamic conditions. Raw measurement accuracies obtained in signal simulator tests are better than 1m for C/A code pseudorange, 1mm for L1 carrier phase, and 10cm/s for L1 Doppler measurements in the absence of environmental error sources such as multipath.

Bill of Materials

The complete bill of materials, list of hardware vendors, and helpful design and building information will be available upon request.

Ongoing

10/18/2002: Finally, we received 10 Orion receivers!

10/08/2002: The navigation and raw data quality tests have been performed for the engineering models. The test procedures are defined by Holt in his masters thesis.

10/07/2002: Two engineering models are delivered for testing.

09/30/2002: The parts are sent to Silicon Hills Design for assembly.

09/09/2002: 20 PCBs for the main board are now in stock. We are ready for assembly!

08/27/2002: PCBPro delivered 20 PCBs for the interface board.

07/26/2002: The main board is in production.

07/22/2002: All the receiver parts except for the PCBs are now in stock at CSR.

07/05/2002: The interface board is in production.

06/26/2002: The site was created.

Publications

Precise Spacecraft Relative Navigation Using Kinematic Inter-Spacecraft State Estimates: T. Ebinuma, O. Montenbruck, and E.G. Lightsey, ION GPS 2002, Portland, Oregon, September 24-27, 2002.

Related Site

Orion GPS receiver development at DLR/GSOC