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Underwater Robots - Gianluca Antonelli.pdf

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4.3 Fault Detection Schemes 85<br />

planar simulation is provided in case of low speed under wave action and a<br />

stuck fin.<br />

+<br />

−<br />

FIS<br />

FD<br />

FTC UUV<br />

high level<br />

Fig. 4.4. Fuzzy fault detection/tolerant control scheme proposed by A.J. Healey:<br />

the FIS (Fuzzy Inference System) block is in charge of isolating faults observed by<br />

the FD (Fault Detection) block between fin stroke, servo error, residual and wave<br />

activity detectors<br />

Amodel-free fault detection method isproposed in [43, 173]: this is based<br />

on the Hotelling T 2 statistic and it is adata-driven approach. The validation<br />

is based on a6-DOFs simulation affected by stern plane jams and rudder<br />

jams.<br />

Amodel-based, integrated heterogeneous knowledge approach is proposed<br />

in [140]. Amulti-dimensional correlation analysis allows to increase the confidence<br />

in the detected fault and to detect also indirectly sensed subsystems.<br />

Some preliminary results with the vehicle RAUVER are also given.<br />

In [1] amodel-based fault detection scheme for thrusters and sensors is<br />

proposed. It has been designed based on the identified model of the 6-thruster<br />

ROV Linotip and it is composed of abank ofsingle-output Luenberger observers.<br />

Its effectiveness is verified bysimulations. Another model-based fault<br />

detection scheme verified bysimulations is provided in [238]. Arobust approach<br />

in[199].<br />

Aneuro-symbolic hybrid system is used in[102] to perform fault diagnosis<br />

on AUVs with learning capability. The method issimulated on the planar<br />

motion ofthe VORTEX mathematical model. Another learning technique is<br />

proposed in [113] and verified bymeans of 6-DOFs simulations. In [284], a<br />

neural network mathematical model is used to set-up aself-diagnosis scheme<br />

of the AUV. Asoftware forhealth monitoringofAUVs’ missions with learning<br />

capabilities is also described in [151].<br />

The work in [39] studies asystematic, quantitative approach inorder to<br />

maximize the mission and return success probabilities. The failed sensor is

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