Carrier Phase Ambiguity Search Constrained by Terrestrial Spatial Data

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Solution Overview

Problem

Existing satellite positioning systems face challenges in resolving integer ambiguities in carrier phase measurements, particularly in non-open-sky environments, leading to inefficiencies in high-precision positioning and satellite signal acquisition.

Innovation Solution

Constraining the satellite positioning system carrier phase integer ambiguity search space using spatial information from terrestrial-based signals, such as range, angle, and position estimates, to reduce the search space and enhance precision.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If the satellite positioning system uses carrier phase measurements for high-precision positioning, then positioning precision is improved, but the integer ambiguity search space becomes excessively large making resolution difficult

Engineering Contradiction:
Improvepositioning precisionVSAvoidsearch space size
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent segments the integer ambiguity resolution problem by dividing the search space into manageable subsets using spatial constraints. Instead of searching the entire ambiguous space, the system partitions it based on geometric relationships between satellites, improving tractability while maintaining precision.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent applies local quality by focusing the search effort on specific regions of the ambiguity space that are most likely to contain the correct integer solution. By identifying and concentrating computational resources on promising local areas rather than uniformly searching all possibilities, the system achieves efficient resolution.

Inventive Principle:
Principle #3Local quality

2Measurement precision

If the system searches the full integer ambiguity space to ensure accurate positioning, then positioning accuracy is maintained, but the time required for signal acquisition and positioning increases

Engineering Contradiction:
Improvepositioning accuracyVSAvoidsignal acquisition time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The patent performs preliminary actions by pre-computing spatial constraints and geometric relationships before the actual integer ambiguity resolution. By preparing constraint information in advance based on satellite ephemeris and receiver position data, the system reduces the computational burden during real-time positioning, enabling faster acquisition without sacrificing accuracy.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent applies partial action by searching only a constrained subset of the full ambiguity space rather than exhaustively searching all possibilities. The spatial constraints eliminate obviously incorrect solutions, allowing the system to achieve sufficient accuracy by examining only the most promising candidates.

Inventive Principle:
Principle #16Partial or excessive action

3Adaptability or versatility

If the system operates in non-open-sky environments with limited satellite visibility, then coverage is maintained, but the integer ambiguity resolution becomes more challenging due to reduced geometric diversity

Engineering Contradiction:
Improveenvironmental coverageVSAvoidambiguity resolution reliability
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The patent introduces spatial dimensionality constraints as an additional degree of freedom for resolving ambiguities. By incorporating three-dimensional geometric relationships between satellites and the receiver, the system compensates for reduced satellite visibility in non-open-sky environments, maintaining reliability through enhanced geometric modeling.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Data Source

PatentUS12487369B2Integer ambiguity search space reduction
Publication Date: 2025.12.02 QUALCOMM INC
  • US12487369B2 patent drawing
  • US12487369B2 patent drawing
  • US12487369B2 patent drawing

AI summary

A method of determining an integer ambiguity search space includes: obtaining, at an apparatus, a code phase measurement of a satellite vehicle signal comprising a pseudorandom noise code and a carrier signal; obtaining, at the apparatus, spatial information corresponding to a wireless terrestrial signal transferred between the apparatus and a terrestrial base station; determining, at the apparatus, a satellite positioning system carrier phase integer ambiguity search space based on the code phase measurement; and constraining a size of the satellite positioning system carrier phase integer ambiguity search space based on the spatial information.