SINS/ANS integration for augmented performance navigation solution using unscented Kalman filtering

Jamshaid Ali; Jiancheng Fang

doi:10.1016/j.ast.2005.11.009

ScienceGate Book Chapters

JOURNAL ARTICLE

SINS/ANS integration for augmented performance navigation solution using unscented Kalman filtering

Jamshaid Ali Jiancheng Fang

Year: 2006 Journal: Aerospace Science and Technology Vol: 10 (3)Pages: 233-238 Publisher: Elsevier BV

DOI: 10.1016/j.ast.2005.11.009

Get Full-Text PDF Get Analytical Report

Keywords:

Kalman filter Inertial navigation system Control theory (sociology) Unscented transform Celestial navigation Transformation (genetics) Covariance Navigation system Nonlinear system Compensation (psychology) Filter (signal processing) Extended Kalman filter Computer science Engineering Invariant extended Kalman filter Artificial intelligence Computer vision Orientation (vector space) Mathematics

Metrics

Cited By

2.37

FWCI (Field Weighted Citation Impact)

Refs

0.93

Citation Normalized Percentile

Is in top 1%

Is in top 10%

Citation History

Topics

Inertial Sensor and Navigation

Physical Sciences → Engineering → Aerospace Engineering

Target Tracking and Data Fusion in Sensor Networks

Physical Sciences → Computer Science → Artificial Intelligence

Geophysics and Gravity Measurements

Physical Sciences → Earth and Planetary Sciences → Oceanography

SINS/ANS integration for augmented performance navigation solution using unscented Kalman filtering

Metrics

Citation History

Topics

Related Documents

SINS/CNS integrated navigation solution using adaptive unscented Kalman filtering

Unscented Kalman Filtering for SINS Attitude Estimation

An Augmented State Robust Unscented Kalman Filtering for Gravity Gradient Matching Navigation

Unscented Kalman Filter for SINS/GPS Integrated Navigation System

GPS/SINS Navigation Data Fusion Using Quaternion Model and Unscented Kalman Filter