Preface; Contents; Part I Spacecraft Instrumentation Scienceand Technology; 1 The Application of the GNSS Receiver in the Third Stage of China Lunar Exploration Program; Abstract; 1.1 Introduction; 1.2 Lunar Mission Availability for GNSS; 1.2.1 Simulation Setting; 1.2.2 Earth&hx2013; Moon&hx2013; Earth Transfer Process GNSS Availability; 1.2.2.1 Earth to Moon Transition Phase; 1.2.2.2 Month to Earth Stage; 1.3 High Sensitivity GNSS Receiver Design; 1.3.1 High Sensitivity GNSS Receiver Scheme Design; 1.3.2 Weak Signal Acquisition Algorithm Design; 1.3.2.1 Weak Signal Acquisition Processing

1.3.2.2 Design Acquisition Processing Parameters1.3.3 Weak Signal Tracking Algorithm Design; 1.3.3.1 Weak Signal Tracking Processing; 1.3.3.2 Design Tracking Processing Parameters; 1.3.4 GNSS Orbit Determination Algorithm Design; 1.4 Conclusion; References; 2 Chang'E-3 DOR Signal Processing and Analysis; Abstract; 2.1 Introduction; 2.2 DOR Signal Processing Method; 2.2.1 Local Correlation Algorithm; 2.2.2 Frequency and Phase Correction Based on Polynomial Fitting; 2.3 Test Data Processing and Analysis; 2.4 Conclusion; References

3 Research on Technique of VLBI Data Correlation Post Processing in Deep Space NavigationAbstract; 3.1 Introduction; 3.2 Questions and Phenomenon Analysis; 3.3 Principle of Correlation Post Process; 3.3.1 Principle of Bandwidth Synthesis Method; 3.3.2 Principle of Calibration Method; 3.3.3 Principle of Subtraction Method; 3.4 Calculating Example and Analysis; 3.5 Conclusions; References; 4 Research on Simulation of Inter-satellite Link Based on the Navigating Constellation; Abstract; 4.1 Introduction; 4.2 Design and Implementation of a Simulating Platform

4.2.1 Constellation and Orbit Determination4.2.2 The Source Module of Telemetry Data; 4.2.3 Network Routing Module; 4.2.4 Data Transmitting and Processing Module; 4.3 Simulating Experiment and Analysis; 4.3.1 Telemetry Time Delay; 4.3.2 Scenario with the Failure of Single Satellite; 4.4 Conclusion; Acknowledgments; References; 5 The Co-simulation of Airborne Stable Platform Based on Adams/Simulink; Abstract; 5.1 Introduction; 5.2 The Co-simulation of Stable Platform Based on Adams and Simulink; 5.3 The Design of Airborne Stabilized Platform Mechanical Module

5.4 The Design of Airborne Stabilized Platform Control Module5.5 The Experiment of Co-simulation Based on Adams/Simulink; 5.6 Conclusions; References; 6 A Study on the Alignment of Platform INS Based on the Rotation Around Azimuth Axis; Abstract; 6.1 Introduction; 6.2 Alignment Scheme Design; 6.3 Dynamic Model and Observation Model of the Alignment; 6.3.1 Dynamic Model and Observation Model; 6.3.2 Observability Analysis; 6.4 Simulation and Analysis; 6.4.1 Simulation; 6.4.2 Compared with the Two-Position Gyrocompass Alignment Method; 6.5 Conclusions; References