Ultratightly Coupled Navigation System Inertial Error Compensation

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Navigation systems face challenges in maintaining accuracy in signal challenging environments due to inertial errors and signal interference, particularly in acquiring and tracking GPS signals, which can lead to instability and prolonged signal re-acquisition times.

Innovation Solution

An extended ultratightly coupled navigation system architecture employing an extended Kalman Filter and Pre-Filter algorithm, combined with an inertial compensation unit and stochastic regulator, to mitigate inertial errors and provide stable and accurate geolocation information, even in indoor and urban environments, by using distributed adaptive algorithms for control and estimation of stochastic processes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If inertial navigation systems are combined with GPS tracking in ultratightly coupled architectures, then tracking accuracy is enhanced, but inertial errors accumulate and degrade navigation accuracy

Engineering Contradiction:
Improvetracking accuracyVSAvoidnavigation accuracy
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The patent implements a feedback mechanism where GPS measurements are used to correct inertial navigation system errors. The system continuously compares inertial predictions with actual GPS measurements and feeds back correction signals to compensate for inertial drift, thereby maintaining navigation accuracy over time despite inertial error accumulation

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent introduces an intermediary correction mechanism that processes both inertial and GPS data separately before combining them. This intermediary layer filters and reconciles the two data streams, using GPS to correct inertial errors while preserving the high-rate inertial navigation output, thus resolving the contradiction between enhanced tracking and maintained accuracy

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If signal processing complexity is increased to maintain accuracy in challenging environments, then position accuracy is improved, but computational intensity and system size increase

Engineering Contradiction:
Improveposition accuracyVSAvoidcomputational intensity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent performs preliminary processing of inertial and GPS data separately before their combination. By pre-processing and organizing the data streams in advance, the system reduces the computational burden during the critical fusion stage, maintaining high position accuracy while lowering overall computational intensity and system complexity

Inventive Principle:
Principle #10Preliminary action

3Reliability

If GPS signal tracking is maintained in interference environments, then navigational information is obtained, but signal acquisition time increases after signal loss

Engineering Contradiction:
Improvesignal trackingVSAvoidsignal recovery time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent prepares the system in advance for signal loss by maintaining inertial navigation capability that can operate independently. When GPS signals are lost or degraded, the pre-prepared inertial system provides immediate continuity of navigational information, cushioning against the time delay that would otherwise occur during signal re-acquisition

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Data Source

PatentUS8725327B2Navigation system and method of obtaining accurate navigational information in signal challenging environments
Publication Date: 2014.05.13 L3HARRIS GLOBAL COMMUNICATIONS INC
  • US8725327B2 patent drawing
  • US8725327B2 patent drawing
  • US8725327B2 patent drawing

AI summary

A present invention embodiment includes a navigation system with a front-end GPS receiver, auxiliary sensors and a digital signal processor providing filtering and other processing. The navigation system enhances a UTC type architecture by employing an inertial compensation unit and a stochastic regulator. The inertial compensation unit compensates for inertial errors within the sensors, while the stochastic regulator applies an optimal stochastic control law to control system operation. The inertial compensation unit and stochastic regulator mitigate instability within the navigation system and provide: the functionality to attain high position accuracy in the sub-meter range that is stable and reliable; an optimal solution evident in the process of signal recovery time after loss and reacquisition, thereby resulting in signal-loss recovery with an order of magnitude improvement; and the ability to mitigate inertial errors that originate in the sensors. The navigation system provides navigation information for indoor and urban environmental conditions.