A Fault-Tolerant Multiple Sensor Fusion Approach Applied to UAV Attitude Estimation

Yu Gu, Jason N. Gross, Matthew B. Rhudy, Kyle Lassak

Research output: Contribution to journalArticle

17 Scopus citations

Abstract

A novel sensor fusion design framework is presented with the objective of improving the overall multisensor measurement system performance and achieving graceful degradation following individual sensor failures. The Unscented Information Filter (UIF) is used to provide a useful tool for combining information from multiple sources. A two-step off-line and on-line calibration procedure refines sensor error models and improves the measurement performance. A Fault Detection and Identification (FDI) scheme crosschecks sensor measurements and simultaneously monitors sensor biases. Low-quality or faulty sensor readings are then rejected from the final sensor fusion process. The attitude estimation problem is used as a case study for the multiple sensor fusion algorithm design, with information provided by a set of low-cost rate gyroscopes, accelerometers, magnetometers, and a single-frequency GPS receiver's position and velocity solution. Flight data collected with an Unmanned Aerial Vehicle (UAV) research test bed verifies the sensor fusion, adaptation, and fault-tolerance capabilities of the designed sensor fusion algorithm.

Original languageEnglish (US)
Article number6217428
JournalInternational Journal of Aerospace Engineering
Volume2016
DOIs
StatePublished - 2016

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Fingerprint Dive into the research topics of 'A Fault-Tolerant Multiple Sensor Fusion Approach Applied to UAV Attitude Estimation'. Together they form a unique fingerprint.

  • Cite this