Force Fight and Its Elimination in a Prototype of a Redundant Direct-Drive Avionic Actuator
| Autor: | Guillaume Krebs, Pierre Estival, Rabia Sehab, Bertrand Barbedette |
|---|---|
| Jazyk: | angličtina |
| Rok vydání: | 2020 |
| Předmět: |
0209 industrial biotechnology
Specific test Computer science Reliability (computer networking) force fight 02 engineering and technology sensors lcsh:Technology law.invention lcsh:Chemistry 020901 industrial engineering & automation 0203 mechanical engineering law permanent magnet synchronous machine Redundancy (engineering) General Materials Science lcsh:QH301-705.5 Instrumentation actuator Fluid Flow and Transfer Processes 020301 aerospace & aeronautics reliability lcsh:T Rotor (electric) redundancy Process Chemistry and Technology General Engineering Control engineering faults Avionics lcsh:QC1-999 Computer Science Applications Power (physics) monitoring lcsh:Biology (General) lcsh:QD1-999 lcsh:TA1-2040 Magnet lcsh:Engineering (General). Civil engineering (General) Actuator position control lcsh:Physics performance |
| Zdroj: | Applied Sciences Volume 10 Issue 23 Applied Sciences, Vol 10, Iss 8492, p 8492 (2020) |
| ISSN: | 2076-3417 |
| DOI: | 10.3390/app10238492 |
| Popis: | Nowadays, in aeronautical applications, rigorous reliability requirements are high constraints for embedded systems. Therefore, material redundancy is adopted to ensure safety whatever operation conditions may be. In the design of a direct-drive actuator for a specific application, redundancy is taken into account using a compound of four three-phase permanent magnet synchronous machines (PMSM). Each two electric machines are mounted in series sharing the same rotor with a common through shaft. The stators of each two electric machines are designed and manufactured as a six-phase machine. For each machine, power supply, sensors, and control loops are independent. In the characterization of the designed actuator and in the validation of its specific control in healthy operation mode and in faulty operation mode, taking into account the force fight phenomenon between the motor lanes, a specific test bench is developed. The aim of this paper is to highlight this phenomenon in faulty operation mode and to develop an easily implementable monitoring architecture, in order to eliminate it. Finally, with the proposed approach of monitoring, the force fight phenomenon is eliminated in faulty operation mode keeping the same performance as in healthy operation mode. |
| Databáze: | OpenAIRE |
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