DocumentCode
115364
Title
Robust estimation with faulty measurements using recursive-RANSAC
Author
Niedfeldt, Peter C. ; Beard, Randal W.
Author_Institution
Electr. & Comput. Eng., Brigham Young Univ., Brigham, UK
fYear
2014
fDate
15-17 Dec. 2014
Firstpage
4160
Lastpage
4165
Abstract
Many autonomous platforms, such as micro air-vehicles, are increasingly relying on cheap, lightweight sensors to improve the low-level state estimation for navigation and control. Unfortunately, these and all sensors have a finite probability of returning spurious measurements that do not follow the classical zero-mean Gaussian models of measurement noise. A classical heuristic used to mitigate the effects of sensor faults is the gated-Kalman filter. We show that the gated- Kalman filter estimate diverges from the true states when the probability of detection is low or when the measurement noise standard deviation increases above the expected value. The main contribution of this paper is to utilize the recently developed recursive-RANSAC algorithm in a feedback loop to robustly estimate the true states when the probability of a sensor fault is high, when the measurement noise characteristics abruptly change, and during brief occlusions of the true signal, while maintaining real-time performance.
Keywords
Kalman filters; autonomous aerial vehicles; estimation theory; feedback; iterative methods; sensors; state estimation; autonomous platforms; faulty measurements; feedback loop; finite probability; gated-Kalman filter; low-level state estimation; measurement noise standard deviation; micro air-vehicles; recursive-RANSAC; robust estimation; sensor faults; state estimation; Clutter; Current measurement; Kalman filters; Logic gates; Noise; Noise measurement; Sensors;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control (CDC), 2014 IEEE 53rd Annual Conference on
Conference_Location
Los Angeles, CA
Print_ISBN
978-1-4799-7746-8
Type
conf
DOI
10.1109/CDC.2014.7040037
Filename
7040037
Link To Document