Detection of Sensor Faults in Small Helicopter UAVs Using Observer/Kalman Filter Identification
Reliability is a critical issue in navigation of unmanned aerial vehicles (UAVs) since there is no human pilot that can react to any abnormal situation. Due to size and cost limitations, redundant sensor schemes and aeronautical-grade navigation sensors used in large aircrafts cannot be installed in...
Main Authors: | Guillermo Heredia, Anibal Ollero |
---|---|
Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2011-01-01
|
Series: | Mathematical Problems in Engineering |
Online Access: | http://dx.doi.org/10.1155/2011/174618 |
Similar Items
-
Cooperative Virtual Sensor for Fault Detection and Identification in Multi-UAV Applications
by: Alejandro Suarez, et al.
Published: (2018-01-01) -
Fault-Tolerant Adaptive Model Predictive Control Using Joint Kalman Filter for Small-Scale Helicopter
by: Castillo, Carlos L
Published: (2008) -
Virtual Sensor for Failure Detection, Identification and Recovery in the Transition Phase of a Morphing Aircraft
by: Guillermo Heredia, et al.
Published: (2010-03-01) -
Multi-Unmanned Aerial Vehicle (UAV) Cooperative Fault Detection Employing Differential Global Positioning (DGPS), Inertial and Vision Sensors
by: Aníbal Ollero, et al.
Published: (2009-09-01) -
Fault detection and performance recovery with Kalman filter-based adaptive observer
by: Chen-Hong Zheng, et al.
Published: (2005)