CSAA/IET International Conference on Aircraft Utility Systems (AUS 2018) 2018
DOI: 10.1049/cp.2018.0138
|View full text |Cite
|
Sign up to set email alerts
|

Sensorless Control Of Dual-Three Phase PMSM Based Aircraft Electric Starter/Generator System Using Model Reference Adaptive System Method

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2023
2023
2023
2023

Publication Types

Select...
4
2

Relationship

0
6

Authors

Journals

citations
Cited by 7 publications
(2 citation statements)
references
References 19 publications
(27 reference statements)
0
2
0
Order By: Relevance
“…Because the stator current can be regulated precisely, this approach has the potential to provide the highest level of rotor positioning precision, while also requiring the least amount of additional complexity in the system. This method's dependability is affected by the existence of the load torque, whose magnitude might induce a shift between the imposed alignment posi-tion and the real one [31,32], as seen in Figure 6. When calculating the stator current of the machine, the MRAS estimator in this scenario utilises two different models.…”
Section: Model Reference Adaptive System (Mras)mentioning
confidence: 99%
“…Because the stator current can be regulated precisely, this approach has the potential to provide the highest level of rotor positioning precision, while also requiring the least amount of additional complexity in the system. This method's dependability is affected by the existence of the load torque, whose magnitude might induce a shift between the imposed alignment posi-tion and the real one [31,32], as seen in Figure 6. When calculating the stator current of the machine, the MRAS estimator in this scenario utilises two different models.…”
Section: Model Reference Adaptive System (Mras)mentioning
confidence: 99%
“…Usually, sensorless control can be classified into two major groups. One is based on the mathematical model of PMSM, suitable for the medium and high speed range, including extended Kalman filter, model reference adaptive system and sliding mode observer [4]. The other is based on the rotor saliency, suitable for low speed range including highfrequency signal injection method.…”
Section: Introductionmentioning
confidence: 99%