Title :
Development of a New Generation Spaceborne GPS Receiver
Author :
Kondoh, Yoshinori ; Ishijima, Yoshiyuki ; Kawano, Isao ; Iwata, Takanori ; Suzuki, Hideto ; Kumagai, Susumu ; Kakinuma, Masahiro ; Eda, Tomoaki ; Kasahara, Masaru
Author_Institution :
Japan Aerosp. Exploration Agency, Tsukuba
Abstract :
We are investigating a new generation spaceborne GPS receiver that can determine a position more precisely, but which is smaller, with lower cost and lower power consumption than a conventional receiver. This new type of spaceborne receiver includes a CMOS silicon on insulator (SOI) chip and adopts a direct sampling approach to process GPS signals. Moreover, this receiver can receive not only legacy GPS signals (L1) but also new civil codes on L2 and L5 frequency bands, for which it has 16 channels each and more than 64 channels in all. Furthermore, this receiver has 6 RF inputs; it can be configured for various applications. In this paper, the concept of the new GPS receiver is explained and the preliminary design results of a receiver signal-processing module are presented. Moreover, we experimentally produced a signal-processing module and evaluated measurement errors of the pseudo-range and carrier phase on each signal. Consequently the validity of this receiver to adopt the direct sampling approach was confirmed. Those results are also described in detail.
Keywords :
CMOS integrated circuits; Global Positioning System; measurement errors; microprocessor chips; radio receivers; signal processing; silicon-on-insulator; CMOS silicon on insulator chip; SOI chip; legacy GPS signals; measurement errors; new generation spaceborne GPS receiver; position determination; power consumption; radio receiver; signal processing module; CMOS process; Costs; Energy consumption; Global Positioning System; Power generation; Radio frequency; Signal design; Signal processing; Signal sampling; Silicon on insulator technology;
Conference_Titel :
Aerospace conference, 2009 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-2621-8
Electronic_ISBN :
978-1-4244-2622-5
DOI :
10.1109/AERO.2009.4839417