By Jiadong Sun, Jingnan Liu, Shiwei Fan, Xiaochun Lu
China satellite tv for pc Navigation convention (CSNC) 2015 Proceedings provides chosen study papers from CSNC2015, held in the course of 13th-15th may possibly in Xian, China. The topic of CSNC2015 is Opening-up, Connectivity and Win-win. those papers speak about the applied sciences and purposes of the worldwide Navigation satellite tv for pc approach (GNSS), and the most recent growth made within the China BeiDou method (BDS) specially. they're divided into 10 issues to compare the corresponding classes in CSNC2015, which largely lined key issues in GNSS. Readers can know about the BDS and hold abreast of the newest advances in GNSS thoughts and functions.
SUN Jiadong is the executive clothier of the Compass/ BDS, and the academician of chinese language Academy of Sciences (CAS); LIU Jingnan is a professor at Wuhan college. FAN Shiwei is a researcher at China satellite tv for pc Navigation place of work; LU Xiaochun is an academician of chinese language Academy of Sciences (CAS).
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Extra resources for China Satellite Navigation Conference (CSNC) 2015 Proceedings: Volume I
Radio Sci 36(3):441–458 2. Sokolovskiy S, Rocken C, Schreiner W et al (2010) On the uncertainty of radio occultation inversions in the lower troposphere. J Geophys Res 115(D22111). 1029/2010JD014058 3. Lohmann MS (2007) Analysis of global positioning system (GPS) radio occultation measurement errors based on Satellite de Aplicaciones Cientiﬁcas-C (SAC-C) GPS radio occultation data recorded in open-loop and phase-locked-loop mode. J Geophys Res 112: D9115. 1029/2006JD007764 4. Sokolovskiy S (2001) Tracking tropospheric radio occultation signals from low Earth orbit.
Error statistics generally 40 X. Liu et al. 3103 ° . 5 3 100 0 -100 Fig. 7807°. 5 0 0 Fig. 0436 °. 5 3 Fig. 5 Jerk = 20 g/s, the tracking performance of PLL 42 X. Liu et al. 1927 °. 5 0 Fig. 2456 includes thermal noise error, Allan deviation and dynamic stress error caused by acceleration. 92 mm, which can better meet the carrier measurement precision is less than 2 mm index, along with the increase of the jerk, when jerk = 5 g/s, the measurement error of this theory has exceeded 2 mm, j = 30 g/s loop is at a complete loss of lock state.
Second, the principles of the carrier phase based attitude determination technique are presented and the characteristics of the CSS are discussed, based on which the technical conditions required for BDS-based attitude determination for the CSS are analyzed. An attitude determination scheme which requires three antennas to be installed on the three CSS’ component cabins respectively is proposed. Next, simulations and analysis on the roll, pitch and yaw angle measurement errors when the CSS is orbiting are conducted.