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Record W2617743738

GPS/INS Integration Based on Recursive Least Square Lattice

2006· article· en· W2617743738 on OpenAlexaboutno aff
Mahmoud ElGizawy, Aboelmagd Noureldin, Naser El‐Sheimy

Bibliographic record

VenueProceedings of the 19th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GNSS 2006) · 2006
Typearticle
Languageen
FieldEngineering
TopicInertial Sensor and Navigation
Canadian institutionsnot available
Fundersnot available
KeywordsGPS/INSGlobal Positioning SystemInertial navigation systemKalman filterControl theory (sociology)Lattice phase equaliserComputer scienceFilter (signal processing)Lattice (music)EstimatorAlgorithmAssisted GPSMathematicsAdaptive filterStatisticsArtificial intelligenceComputer visionGeometryPhysics
DOInot available

Abstract

fetched live from OpenAlex

The integration of both the Global Positioning System (GPS) and Inertial Navigation System (INS) has several navigation and positioning applications. Both systems have their unique features and shortcomings. Therefore, their integration offers robust navigation solution. This paper introduces a novel multi-sensor system integration using Recursive Least Square Lattice (RLSL) filter. The proposed system has a similar structure to the widely used Kalman filter. However, it has the major advantage of working without the need of neither dynamic nor stochastic models. Furthermore, no prior information about the covariance information of INS and GPS is required. The RLSL process includes both the lattice predictor and the joint process estimator. The lattice predictor has a modular structure, which consists of a number of individual stages. Each stage has the appearance of a lattice. This lattice structure allows the simultaneous implementation of one forward and one backward prediction error filters. The forward prediction error is the difference between the input (e.g. INS velocity) and its one-step forward prediction value, which is obtained using a number of past tap inputs equivalent to the filter order. Similarly, the backward prediction error is the difference between the last tap input to the filter and its backward prediction value, which is based on the following tap inputs to the filter. The final forward and backward prediction errors can be determined by moving stage by stage through the lattice predictor. In this study, loosely coupled GPS/INS architecture is adopted and only GPS velocity updates are used. The INS input signal represented by the input sequence has a direct relationship with backward prediction errors. This allows estimating some desired response from a linear combination of the backward prediction errors. The backward prediction errors are uncorrelated and orthogonal random variables, with a diagonal correlation matrix. Therefore, the desired signal (corresponding to the GPS velocity) contained in the input sequence can be estimated throughout the joint process estimator from the backward prediction errors whose tap weights are the regression coefficients, similar to Kalman gain. These regression coefficients are tuned recursively in the update mode utilizing the GPS velocity components. The performance of the proposed RLSL module for GPS/INS integration is examined with a tactical grade system through a field test. The field test was conducted in Calgary (Alberta, Canada) in a land vehicle involving a NovAtel OEM4 GPS receiver and a tactical grade INS system (the Honeywell HG1700). The proposed system is examined during the availability of the GPS signal and with intentionally introduced GPS signal outages. The results indicate that the proposed RLSL system is indeed robust in providing reliable modeless INS/GPS integration module.

Fetched live from OpenAlex and de-inverted. Abstracts are not stored in this database: the inverted indexes are 8.6 GB of the frame’s 9.3 GB of text, and the host has 13 GB free.

How this classification was reachedexpand

Full frame distilled prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. Learned from the 10,348 direct Codex labels and 10,348 direct Gemma labels. Candidate is the union of thresholded teacher heads; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels or direct frontier model labels.

metaresearch head score (Codex)0.001
metaresearch head score (Gemma)0.001
Version: codex-gemma-dda1882f352aValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Bench or experimental · Consensus signal: Bench or experimental
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.145
Threshold uncertainty score0.600

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0010.001
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.001
Science and technology studies0.0000.000
Scholarly communication0.0000.000
Open science0.0010.000
Research integrity0.0000.000
Insufficient payload (model declined to judge)0.0000.000

Machine scores (provisional)

The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.

Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.

Opus teacher head0.009
GPT teacher head0.231
Teacher spread0.222 · how far apart the two teachers sit on this one work
Validation statusscore_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it

Classification

machine, unvalidated

Machine predicted; a candidate call from one teacher head, not a consensus.

The models applied no category: nothing in the taxonomy fit this work.
Study designBench or experimental
Domainnot available
GenreEmpirical

How this classification was reached, model by model and score by score, is at the end of the page under "How this classification was reached".

Quick stats

Citations0
Published2006
Admission routes1
Has abstractyes

Explore more

Same venueProceedings of the 19th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GNSS 2006)Same topicInertial Sensor and NavigationFrench-language works237,207