Related Experiment Video
Updated: Mar 15, 2026

Continuous-Wave Propagation Channel-Sounding Measurement System - Testing, Verification, and Measurements
Published on: June 25, 2021
Weak and Dynamic GNSS Signal Tracking Strategies for Flight Missions in the Space Service Volume.
Shuai Jing1, Xingqun Zhan2, Baoyu Liu3
1School of Aeronautics and Astronautics, Shanghai Jiao Tong University, No. 800 Dongchuan Road, Shanghai 200240, China. lightning95@sjtu.edu.cn.
This study enhances space navigation by improving Global Navigation Satellite System (GNSS) receivers. New adaptive Kalman filter and INS-assisted strategies improve tracking in weak-signal and high-dynamic environments.
Area of Science:
- Space Navigation
- Satellite Systems Engineering
- Signal Processing
Background:
- Space navigation using Global Navigation Satellite Systems (GNSS) faces challenges with weak signals and high dynamics in the Space Service Volume (SSV).
- Conventional third-order phase-locked loop (PLL) architectures in onboard GNSS receivers are insufficient for these demanding conditions.
- Maintaining signal lock is critical for accurate positioning and trajectory determination in space missions.
Purpose of the Study:
- To address the limitations of conventional GNSS receivers in weak-signal and high-dynamic space environments.
- To introduce and evaluate novel tracking strategies for enhanced GNSS performance in the SSV.
- To improve the robustness and reliability of space navigation systems.
Main Methods:
- An adaptive four-state Kalman filter (KF) algorithm was developed to optimize loop noise bandwidth by adaptively adjusting filter gain based on signal power and line-of-sight (LOS) dynamics.
- An open-loop tracking strategy, aided by an Inertial Navigation System (INS), was proposed to maintain signal lock in challenging environments.
- The traditional maximum likelihood estimation (MLE) method was modified non-coherently by reconstructing the likelihood cost function.
Main Results:
- The adaptive four-state KF-based strategy demonstrated effectiveness under non-maneuvering conditions, optimizing loop performance.
- The INS-assisted open-loop tracking strategy proved advantageous during maneuvering conditions, maintaining reliable tracking.
- Computer simulations validated the performance improvements of both proposed strategies under different mission scenarios.
Conclusions:
- The adaptive KF strategy offers significant improvements for GNSS receivers in stable space trajectories.
- INS-assisted methods are crucial for robust GNSS tracking during dynamic orbital maneuvers.
- These advancements enhance the capabilities of GNSS for future space navigation applications.
Related Concept Videos
Types of Global Positioning System Surveys
Errors in Global Positioning System
Field Application of Global Positioning System
Introduction to Global Positioning System
Circular Orbits and Critical Velocity for Satellites
Nicolaus Copernicus (1473-1543) first suggested that the Earth and all other planets orbit the Sun in...
Derivatives of Inverse Trigonometric Functions

