Tightly Coupled GPS/INS/CCD Integration Based on GPS Carrier Phase Velocity Update
暂无分享,去创建一个
[1] Donghyun Kim,et al. Instantaneous real-time cycle-slip correction for quality control of GPS carrier-phase measurements , 2002 .
[2] Arthur Gelb,et al. Applied Optimal Estimation , 1974 .
[3] C. Jekeli,et al. GPS phase accelerations for moving-base vector gravimetry , 1997 .
[4] George M. Siouris,et al. Aerospace Avionics Systems: A Modern Synthesis , 1993 .
[5] C. Jekeli. Inertial navigation systems with geodetic applications , 2000 .
[6] D. A. Grejner-Brzezinska,et al. GPS error modeling and OTF ambiguity resolution for high-accuracy GPS/INS integrated system , 1998 .
[7] Gérard Lachapelle,et al. DGPS High Accuracy Aircraft Velocity Determination Using Doppler Measurements , 1997 .
[8] Gérard Lachapelle,et al. DGPS Kinematic Carrier Phase Signal Simulation Analysis for Precise Aircraft Velocity Determination , 1997 .
[9] I. Bar-Itzhack,et al. Control theoretic approach to inertial navigation systems , 1988 .
[10] Charles K. Toth,et al. Bridging GPS Gaps in Urban Canyons: Can ZUPT Really Help? , 2001 .