Low-Orbit Satellite Relay for High-Accuracy Navigation Positioning
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Solution Overview
Problem
Existing satellite navigation systems face challenges in achieving high positioning accuracy due to the high cost and complexity of high-orbit satellites, which require expensive atomic clocks, and the need for a large number of low-orbit satellites to compensate for signal reception issues.
Innovation Solution
A low-orbit satellite system that relays signals from high-orbit satellites to a ground receiving unit, using an antenna unit, transmitting unit, and control unit to control signal reception and transmission, allowing for high positioning accuracy without the need for expensive payloads on the low-orbit satellites.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Measurement precision
If high-orbit satellites with atomic clocks are used, then positioning accuracy is improved, but system cost and device complexity increase exponentially
Solution Approach 1:
The patent introduces low-orbit satellites as intermediary relay nodes between high-orbit satellites and ground receiving units. The low-orbit satellites receive signals from high-orbit satellites and relay them to ground, enabling positioning accuracy improvement without requiring expensive atomic clocks on every satellite. This mediator approach allows the system to leverage high-orbit satellite signals while using simpler, lower-cost low-orbit platforms.
Solution Approach 2:
The patent creates a signal copying mechanism where low-orbit satellites receive and retransmit signals from high-orbit satellites. Instead of requiring each satellite to generate its own high-precision timing signals with atomic clocks, the system copies the master clock signals from high-orbit satellites to multiple low-orbit relay satellites, distributing the timing reference throughout the network at minimal cost.
2Measurement precision
If low-orbit satellites are used to increase satellite count, then signal reception quality improves, but the number of satellites required increases to 400 or more
Solution Approach 1:
The patent merges the advantages of both high-orbit and low-orbit satellite systems by combining high-orbit satellites (which provide stable, high-precision timing signals) with low-orbit satellites (which provide better signal reception geometry and coverage). This hybrid approach consolidates the functions of having many low-orbit satellites into a smaller network that leverages the strengths of both orbital levels, reducing the total satellite count from 400+ to a manageable number.
Solution Approach 2:
The low-orbit satellites in the patent serve multiple functions: they act as signal relays from high-orbit satellites, provide additional geometric diversity for positioning, and extend coverage areas. This multi-functionality allows each low-orbit satellite to contribute to multiple system objectives simultaneously, reducing the total number of satellites needed compared to a dedicated low-orbit constellation.
3Object-affected harmful factors
If high-orbit satellites are used, then Doppler effect is reduced, but signal reception time becomes shorter than multipath error cycle
Solution Approach 1:
The low-orbit satellites serve as intermediary nodes that receive the stable, low-Doppler signals from high-orbit satellites and retransmit them with enhanced geometric characteristics. This intermediary approach allows the system to benefit from the low Doppler effect of high-orbit satellites while overcoming the limited reception time issue by using the lower orbital altitude of relay satellites to provide better signal geometry and longer effective observation periods.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
This approach enables high-accuracy positioning at a lower cost by using existing high-orbit satellites, reducing the number of satellites required and minimizing signal interference, while maintaining high positioning accuracy.
Implementation Method 1
an antenna unit configured to receive a signal of the high-orbit satellite
Implementation Method 2
a transmitting unit configured to receive the signal from the antenna unit and transmit the signal to the receiving unit
Data Source
AI summary
The present disclosure relates to a satellite system, and more particularly, to a satellite navigation system with high positioning accuracy. According to a low-orbit satellite, a satellite system including the same, and a control method thereof according to the present disclosure, a low-orbit satellite with high positioning accuracy is applied, but in order to reduce costs, the low-orbit satellite relays a signal from the existing high-orbit satellite and transmits the relayed signal to a signal receiving unit, thereby positioning of the receiving unit with high accuracy at low cost.


