GNSS Correction Messaging Using Zenith-Referenced Compression

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Solution Overview

Problem

The increasing demand for bandwidth in global navigation satellite system (GNSS) data transmission, particularly in real-time kinematic (RTK) positioning applications, exceeds the available bandwidth, especially in scenarios where expanding bandwidth is costly or not feasible, necessitating a more efficient data transmission method.

Innovation Solution

The Compressed Measurement Record-Extended (CMRx) technique reduces the amount of data transmitted by sending only ambiguous observation data, utilizing knowledge of signal structure and constellation geometry to eliminate redundant information, and employing algorithms to reconstruct necessary data at the recipient, thereby minimizing bandwidth usage while ensuring full data reconstruction.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If complete GNSS observation data is transmitted to ensure full information availability, then data integrity is maintained, but bandwidth consumption increases

Engineering Contradiction:
Improvedata integrityVSAvoidbandwidth consumption
Core Design Contradiction:
ReliabilityVSQuantity of substance

Solution Approach 1:

The patent extracts and transmits only the essential ambiguous observation data (code phase and carrier phase measurements) while eliminating redundant information such as satellite ephemeris, clock corrections, and atmospheric models that can be obtained from other sources or reconstructed at the receiver end

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The receiver reconstructs the complete observation data by combining the transmitted ambiguous data with locally stored satellite almanac information and atmospheric models, creating a full replica of the original observation record without transmitting all original data

Inventive Principle:
Principle #26Copying

2Measurement precision

If more satellites are included in the constellation to improve positioning accuracy, then positioning precision increases, but data transmission bandwidth requirements increase

Engineering Contradiction:
Improvepositioning accuracyVSAvoiddata transmission volume
Core Design Contradiction:
Measurement precisionVSQuantity of substance

Solution Approach 1:

The patent changes the parameter representation by encoding satellite identifiers using differential encoding where only changes in satellite PRN numbers are transmitted, and by representing observation data as ambiguities relative to a reference epoch rather than absolute values, significantly reducing the data volume per satellite

Inventive Principle:
Principle #35Parameter changes

3Speed

If real-time data transmission is implemented to enable dynamic positioning, then positioning speed is improved, but bandwidth requirements exceed available capacity

Engineering Contradiction:
Improvepositioning speedVSAvoidbandwidth availability
Core Design Contradiction:
SpeedVSQuantity of substance

Solution Approach 1:

The patent implements periodic transmission of ambiguous observation data at standardized epochs (e.g., every second) rather than continuous transmission, allowing the system to maintain real-time positioning capability while utilizing bandwidth efficiently through regular, predictable data bursts

Inventive Principle:
Principle #19Periodic action

Solution Approach 2:

The receiver performs preliminary processing by combining transmitted ambiguous data with pre-stored satellite almanac information and atmospheric models before final position calculation, enabling real-time positioning with minimal additional data transmission

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS8044849B2Method of compactly communicating ionospheric and tropospheric corrections in a network of global navigation system satellite receivers
Publication Date: 2011.10.25 TRIMBLE NAVIGATION LTD
  • US8044849B2 patent drawing
  • US8044849B2 patent drawing
  • US8044849B2 patent drawing

AI summary

A method of communicating corrections for information related to satellite signals among global navigation satellite system (GNSS) receivers is described. An ionosphere correction for ionosphere signal path delay is determined for a first satellite. This ionosphere correction is then compared to an ionosphere correction for ionosphere signal path delay for a satellite assumed to be directly over the receiver. The receiver then sends a message which includes only the difference between the ionosphere correction for the actual observation and the ionosphere correction for a satellite assumed to be at the zenith.