Design of airborne actuator control electronics based on FPGA
Design of airborne actuator control electronics based on FPGA
- Author(s): L. Li 1 ; P. Guo 1 ; S. Wei 1 ; X. Wang 1 ; Z. Xue 1 ; Z. Nie 1
- DOI: 10.1049/icp.2021.0351
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- Author(s): L. Li 1 ; P. Guo 1 ; S. Wei 1 ; X. Wang 1 ; Z. Xue 1 ; Z. Nie 1
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View affiliations
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Affiliations:
1:
Beijing Institute of Precision Mechatronics and Controls , No.1 South Da Hong Men Road, Beijing, China
Source:
CSAA/IET International Conference on Aircraft Utility Systems (AUS 2020),
2021
p.
665 – 671
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Affiliations:
1:
Beijing Institute of Precision Mechatronics and Controls , No.1 South Da Hong Men Road, Beijing, China
- Conference: CSAA/IET International Conference on Aircraft Utility Systems (AUS 2020)
- DOI: 10.1049/icp.2021.0351
- ISBN: 978-1-83953-419-5
- Location: Online Conference
- Conference date: 18-21 September 2020
- Format: PDF
An integrated airborne Actuator Control Electronics (ACE) based on FPGA of the Electro-Mechanical Actuator has been designed to control the cargo door motion.
This paper illustrates the constitution of the ACE and introduces the designing method of parallel processing logic. In the experimental part, a prototype motor driver is designed and tested on loading platform with linear actuator. The results show that the cargo door is precisely controlled for closing, the amplitudes of DC bus current and phase current are within the specified range, working states and their transition logics are reasonable.
Inspec keywords: field programmable gate arrays; motion control; electromechanical actuators
Subjects: Electromechanical actuators; Logic and switching circuits; Control gear and apparatus; Spatial variables control; Logic circuits