Model based approaches for condition monitoring

Author(s):  
R. Goodall

Energies ◽  
2017 ◽  
Vol 10 (9) ◽  
pp. 1266 ◽  
Author(s):  
Md Rahman ◽  
Sohel Anwar ◽  
Afshin Izadian


2019 ◽  
Vol 120 ◽  
pp. 630-641 ◽  
Author(s):  
M. González ◽  
O. Salgado ◽  
X. Hernandez ◽  
J. Croes ◽  
B. Pluymers ◽  
...  


Actuators ◽  
2021 ◽  
Vol 10 (9) ◽  
pp. 230
Author(s):  
Gianpietro Di Rito ◽  
Benedetto Luciano ◽  
Nicola Borgarelli ◽  
Marco Nardeschi

The work deals with the development of deterministic model-based condition-monitoring algorithms for an electromechanical flight control actuator with fault-tolerant architecture, in which two permanent magnets synchronous motors are coupled with differential ball screws in speed-summing paradigm, so that the system can operate even after a motor fault, an inverter fault or a mechanical jamming. To demonstrate the potential applicability of the system for safety-critical aerospace applications, the failure transients related to major fault modes have to be characterised and analysed. By focusing the attention to jamming faults, a detailed nonlinear model of the actuator is developed from physical first principles and experimentally validated in both time and frequency domains for normal condition and with different types of jamming. The validated model is then used to design the condition-monitoring algorithms and to characterize the system failure transient, by simulating mechanical blocks in different locations of the transmission. The operability after the fault, obtained via fault-tolerant control strategy and position regulator reconfiguration, is also verified, by highlighting and discussing possible enhancements and criticalities.



2012 ◽  
Vol 45 (20) ◽  
pp. 618-623 ◽  
Author(s):  
Daniel Hast ◽  
Markus Gottfried ◽  
Rolf Findeisen


Author(s):  
S. Windmann ◽  
J. Eickmeyer ◽  
F. Jungbluth ◽  
J. Badinger ◽  
O. Niggemann


2004 ◽  
Vol 25 (1) ◽  
pp. 65-75 ◽  
Author(s):  
R A Buswell ◽  
J A Wright


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