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Research on HILS Technology Applied on Aircraft Electric Braking System.

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Τίτλος: Research on HILS Technology Applied on Aircraft Electric Braking System.
Συγγραφείς: Zhou, Suying, Lin, Hui, Li, Bingqiang
Πηγή: Journal of Electrical & Computer Engineering; 10/11/2017, p1-14, 14p
Θεματικοί όροι: Airplane brakes, Technological innovations in the aircraft industry, Hardware-in-the-loop simulation, Engineering systems -- Computer simulation, Algorithms
Περίληψη: On the basis of analyzing the real-time feature of hardware-in-the-loop simulation of aircraft braking system, a new simulation method based on MATLAB/RTW (Real-Time Workshop) and DSP is introduced. The purpose of this research is to develop a digital control unit with antilock brake system control algorithm for aircraft braking system using HILS. DSP is used as simulator. Using this method, a detailed mathematical modeling of system is proposed first. Studies on reducing sampling time with model simplification and modeling for applying to I/O interface of DSP and HILS are conducted. Compared with other methods, this method is low cost and convenient to implement. By using these methods, we can complete HIL simulation of aircraft braking under various experimental conditions, modify its control laws, and test its braking performance. The results have demonstrated that this platform has high reliability. The algorithm is verified by real-time closed loop test with HILS system and the results are presented. [ABSTRACT FROM AUTHOR]
Copyright of Journal of Electrical & Computer Engineering is the property of Wiley-Blackwell and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)
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Header DbId: edb
DbLabel: Complementary Index
An: 125596988
RelevancyScore: 861
AccessLevel: 6
PubType: Academic Journal
PubTypeId: academicJournal
PreciseRelevancyScore: 861.363525390625
IllustrationInfo
Items – Name: Title
  Label: Title
  Group: Ti
  Data: Research on HILS Technology Applied on Aircraft Electric Braking System.
– Name: Author
  Label: Authors
  Group: Au
  Data: <searchLink fieldCode="AR" term="%22Zhou%2C+Suying%22">Zhou, Suying</searchLink><br /><searchLink fieldCode="AR" term="%22Lin%2C+Hui%22">Lin, Hui</searchLink><br /><searchLink fieldCode="AR" term="%22Li%2C+Bingqiang%22">Li, Bingqiang</searchLink>
– Name: TitleSource
  Label: Source
  Group: Src
  Data: Journal of Electrical & Computer Engineering; 10/11/2017, p1-14, 14p
– Name: Subject
  Label: Subject Terms
  Group: Su
  Data: <searchLink fieldCode="DE" term="%22Airplane+brakes%22">Airplane brakes</searchLink><br /><searchLink fieldCode="DE" term="%22Technological+innovations+in+the+aircraft+industry%22">Technological innovations in the aircraft industry</searchLink><br /><searchLink fieldCode="DE" term="%22Hardware-in-the-loop+simulation%22">Hardware-in-the-loop simulation</searchLink><br /><searchLink fieldCode="DE" term="%22Engineering+systems+--+Computer+simulation%22">Engineering systems -- Computer simulation</searchLink><br /><searchLink fieldCode="DE" term="%22Algorithms%22">Algorithms</searchLink>
– Name: Abstract
  Label: Abstract
  Group: Ab
  Data: On the basis of analyzing the real-time feature of hardware-in-the-loop simulation of aircraft braking system, a new simulation method based on MATLAB/RTW (Real-Time Workshop) and DSP is introduced. The purpose of this research is to develop a digital control unit with antilock brake system control algorithm for aircraft braking system using HILS. DSP is used as simulator. Using this method, a detailed mathematical modeling of system is proposed first. Studies on reducing sampling time with model simplification and modeling for applying to I/O interface of DSP and HILS are conducted. Compared with other methods, this method is low cost and convenient to implement. By using these methods, we can complete HIL simulation of aircraft braking under various experimental conditions, modify its control laws, and test its braking performance. The results have demonstrated that this platform has high reliability. The algorithm is verified by real-time closed loop test with HILS system and the results are presented. [ABSTRACT FROM AUTHOR]
– Name: Abstract
  Label:
  Group: Ab
  Data: <i>Copyright of Journal of Electrical & Computer Engineering is the property of Wiley-Blackwell and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)
PLink https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&db=edb&AN=125596988
RecordInfo BibRecord:
  BibEntity:
    Identifiers:
      – Type: doi
        Value: 10.1155/2017/3503870
    Languages:
      – Code: eng
        Text: English
    PhysicalDescription:
      Pagination:
        PageCount: 14
        StartPage: 1
    Subjects:
      – SubjectFull: Airplane brakes
        Type: general
      – SubjectFull: Technological innovations in the aircraft industry
        Type: general
      – SubjectFull: Hardware-in-the-loop simulation
        Type: general
      – SubjectFull: Engineering systems -- Computer simulation
        Type: general
      – SubjectFull: Algorithms
        Type: general
    Titles:
      – TitleFull: Research on HILS Technology Applied on Aircraft Electric Braking System.
        Type: main
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          Name:
            NameFull: Zhou, Suying
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            NameFull: Lin, Hui
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            NameFull: Li, Bingqiang
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          Dates:
            – D: 11
              M: 10
              Text: 10/11/2017
              Type: published
              Y: 2017
          Identifiers:
            – Type: issn-print
              Value: 20900147
          Titles:
            – TitleFull: Journal of Electrical & Computer Engineering
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