| Literature DB >> 22969386 |
Oresti Banos1, Miguel Damas, Hector Pomares, Ignacio Rojas.
Abstract
The main objective of fusion mechanisms is to increase the individual reliability of the systems through the use of the collectivity knowledge. Moreover, fusion models are also intended to guarantee a certain level of robustness. This is particularly required for problems such as human activity recognition where runtime changes in the sensor setup seriously disturb the reliability of the initial deployed systems. For commonly used recognition systems based on inertial sensors, these changes are primarily characterized as sensor rotations, displacements or faults related to the batteries or calibration. In this work we show the robustness capabilities of a sensor-weighted fusion model when dealing with such disturbances under different circumstances. Using the proposed method, up to 60% outperformance is obtained when a minority of the sensors are artificially rotated or degraded, independent of the level of disturbance (noise) imposed. These robustness capabilities also apply for any number of sensors affected by a low to moderate noise level. The presented fusion mechanism compensates the poor performance that otherwise would be obtained when just a single sensor is considered.Entities:
Keywords: accelerometer; activity recognition; additive noise; metaclassifier; rotational noise; sensor fusion
Mesh:
Year: 2012 PMID: 22969386 PMCID: PMC3436015 DOI: 10.3390/s120608039
Source DB: PubMed Journal: Sensors (Basel) ISSN: 1424-8220 Impact factor: 3.576
Figure 1.SWNC general structure for a problem with N classes and M nodes.
Figure 2.Effect of the rotational and additive noise. X-axis (green) and Y-axis (blue) accelerations recorded through the ankle located sensor when (a) walking and (b) sitting. Legend: ‘Original’ ≡ raw signals, ‘φ = θ = ψ’ ≡ data with rotational noise, ‘σ’ ≡ data with additive noise.
Figure 3.Effect of the (a) rotational and (b) additive noise when the sensors are separately used. The error bars along the curves correspond to the accuracy standard deviation.
Figure 4.Effect of the (a) rotational and (b) additive noise when the sensor fusion approach is considered. S identifies the number of sensors simultaneously disturbed by the respective noise.