Research on HILS Technology Applied on Aircraft Electric Braking System
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...
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| Format: | Article |
| Language: | English |
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Wiley
2017-01-01
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| Series: | Journal of Electrical and Computer Engineering |
| Online Access: | http://dx.doi.org/10.1155/2017/3503870 |
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| _version_ | 1832560729790611456 |
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| author | Suying Zhou Hui Lin Bingqiang Li |
| author_facet | Suying Zhou Hui Lin Bingqiang Li |
| author_sort | Suying Zhou |
| collection | DOAJ |
| description | 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. |
| format | Article |
| id | doaj-art-46eded1ef9c9458da53a14da7e0f1ba5 |
| institution | Kabale University |
| issn | 2090-0147 2090-0155 |
| language | English |
| publishDate | 2017-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | Journal of Electrical and Computer Engineering |
| spelling | doaj-art-46eded1ef9c9458da53a14da7e0f1ba52025-02-03T01:26:51ZengWileyJournal of Electrical and Computer Engineering2090-01472090-01552017-01-01201710.1155/2017/35038703503870Research on HILS Technology Applied on Aircraft Electric Braking SystemSuying Zhou0Hui Lin1Bingqiang Li2School of Automation, Northwest Polytechnical University, Xi’an, ChinaSchool of Automation, Northwest Polytechnical University, Xi’an, ChinaSchool of Automation, Northwest Polytechnical University, Xi’an, ChinaOn 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.http://dx.doi.org/10.1155/2017/3503870 |
| spellingShingle | Suying Zhou Hui Lin Bingqiang Li Research on HILS Technology Applied on Aircraft Electric Braking System Journal of Electrical and Computer Engineering |
| title | Research on HILS Technology Applied on Aircraft Electric Braking System |
| title_full | Research on HILS Technology Applied on Aircraft Electric Braking System |
| title_fullStr | Research on HILS Technology Applied on Aircraft Electric Braking System |
| title_full_unstemmed | Research on HILS Technology Applied on Aircraft Electric Braking System |
| title_short | Research on HILS Technology Applied on Aircraft Electric Braking System |
| title_sort | research on hils technology applied on aircraft electric braking system |
| url | http://dx.doi.org/10.1155/2017/3503870 |
| work_keys_str_mv | AT suyingzhou researchonhilstechnologyappliedonaircraftelectricbrakingsystem AT huilin researchonhilstechnologyappliedonaircraftelectricbrakingsystem AT bingqiangli researchonhilstechnologyappliedonaircraftelectricbrakingsystem |