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Published on: June 25, 2021
A Novel Linear Model Based on Code Approximation for GNSS/INS Ultra-Tight Integration System.
Zhe Yan1, Xiyuan Chen1, Xinhua Tang1
1Key Laboratory of Micro-Inertial Instrument and Advanced Navigation Technology, Ministry of Education, School of Instrument Science and Engineering, Southeast University, Nanjing 210096, China.
This study introduces a new model for global navigation satellite system (GNSS)/inertial navigation system (INS) integration, improving positioning accuracy and stability. The novel approach enhances performance, especially during unstable tracking loops, by reducing code errors.
Area of Science:
- Navigation Systems Engineering
- Satellite Navigation
- Inertial Navigation
Background:
- Ultra-tightly coupled GNSS/INS navigation systems are superior but face challenges with complex, nonlinear observation models.
- Existing models based on I/Q measurements can be highly complex, impacting system performance and stability.
Purpose of the Study:
- To develop a novel, more stable, and accurate navigation model for GNSS/INS ultra-tight integration.
- To address inherent nonlinearities and improve positioning accuracy and convergence characteristics.
Main Methods:
- A new nonlinear model and linearization method are proposed, retaining second-order components for enhanced precision.
- A novel method to approximate code-phase is introduced to mitigate positioning errors from code-loop deviation without new measurements.
Main Results:
- The proposed model demonstrates higher positioning accuracy and better convergence compared to traditional methods.
- The code-phase approximation significantly reduces the impact of code errors, particularly in unstable tracking loop conditions.
Conclusions:
- The developed model and linearization technique offer improved integrity and stability for GNSS/INS ultra-tight integration.
- Experimental validation confirms the effectiveness and superiority of the proposed methods for enhanced navigation performance.
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