Modeling and control of helicopter flight control system with a controllable Semi-rotary fluid viscous damper
To improve the handling comfort of Helicopter Flight Control System (HFCS), an adaptive particle swarm optimization optimized variable universe fuzzy proportional-integral-derivative (APSO-VUFPID) strategy for damping force control is proposed. First of all, by the results of the controllable semi-r...
| Main Authors: | , , , , , , |
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| Format: | Article |
| Language: | English |
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Elsevier
2022-12-01
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| Series: | Alexandria Engineering Journal |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S1110016822004161 |
| _version_ | 1797978738233704448 |
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| author | Xiaoyan Cao Min Yu Jin Zhou Chaowu Jin Yuanping Xu Xinxing Guo Yunzhi Wang |
| author_facet | Xiaoyan Cao Min Yu Jin Zhou Chaowu Jin Yuanping Xu Xinxing Guo Yunzhi Wang |
| author_sort | Xiaoyan Cao |
| collection | DOAJ |
| description | To improve the handling comfort of Helicopter Flight Control System (HFCS), an adaptive particle swarm optimization optimized variable universe fuzzy proportional-integral-derivative (APSO-VUFPID) strategy for damping force control is proposed. First of all, by the results of the controllable semi-rotary fluid viscous damper (CSFVD) mechanical tests, a hyperbolic tangent model is developed. Afterwards, an equivalent model of HFCS is established. In the next part, aiming at improving the vibration suppression performance of the joystick system, an APSO-VUFPID is proposed to generate the desired damping force in real-time. Finally, numerical simulation and experimental tests are carried out to verify the vibration reduction effect of the proposed APSO-VUFPID method with respect to passive, proportional-integral-derivative (PID), adaptive particle swarm optimization optimized proportional-integral-derivative (APSO-PID) and adaptive particle swarm optimization optimized fuzzy proportional-integral-derivative (APSO-FPID) methods. The results show that the hyperbolic tangent model can accurately describe the nonlinear mechanical characteristics of the CSFVD. Moreover, under the proposed APSO-VUFPID control method, the amplitude of acceleration and velocity of the joystick system are smaller than those obtained from passive, PID, APSO-PID and APSO-FPID methods. Therefore, the proposed APSO-VUFPID controller has better handling comfort compared to passive, PID, APSO-PID and APSO-FPID controllers and can be employed in real applications. |
| first_indexed | 2024-04-11T05:27:47Z |
| format | Article |
| id | doaj.art-06de3b54947d4e6bafc9243c7edb0b4b |
| institution | Directory Open Access Journal |
| issn | 1110-0168 |
| language | English |
| last_indexed | 2024-04-11T05:27:47Z |
| publishDate | 2022-12-01 |
| publisher | Elsevier |
| record_format | Article |
| series | Alexandria Engineering Journal |
| spelling | doaj.art-06de3b54947d4e6bafc9243c7edb0b4b2022-12-23T04:39:40ZengElsevierAlexandria Engineering Journal1110-01682022-12-0161121272512738Modeling and control of helicopter flight control system with a controllable Semi-rotary fluid viscous damperXiaoyan Cao0Min Yu1Jin Zhou2Chaowu Jin3Yuanping Xu4Xinxing Guo5Yunzhi Wang6College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCorresponding authors.; College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCorresponding authors.; College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaCollege of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaTo improve the handling comfort of Helicopter Flight Control System (HFCS), an adaptive particle swarm optimization optimized variable universe fuzzy proportional-integral-derivative (APSO-VUFPID) strategy for damping force control is proposed. First of all, by the results of the controllable semi-rotary fluid viscous damper (CSFVD) mechanical tests, a hyperbolic tangent model is developed. Afterwards, an equivalent model of HFCS is established. In the next part, aiming at improving the vibration suppression performance of the joystick system, an APSO-VUFPID is proposed to generate the desired damping force in real-time. Finally, numerical simulation and experimental tests are carried out to verify the vibration reduction effect of the proposed APSO-VUFPID method with respect to passive, proportional-integral-derivative (PID), adaptive particle swarm optimization optimized proportional-integral-derivative (APSO-PID) and adaptive particle swarm optimization optimized fuzzy proportional-integral-derivative (APSO-FPID) methods. The results show that the hyperbolic tangent model can accurately describe the nonlinear mechanical characteristics of the CSFVD. Moreover, under the proposed APSO-VUFPID control method, the amplitude of acceleration and velocity of the joystick system are smaller than those obtained from passive, PID, APSO-PID and APSO-FPID methods. Therefore, the proposed APSO-VUFPID controller has better handling comfort compared to passive, PID, APSO-PID and APSO-FPID controllers and can be employed in real applications.http://www.sciencedirect.com/science/article/pii/S1110016822004161Fuzzy PIDVariable universeAPSOFluid damperParametric modeling |
| spellingShingle | Xiaoyan Cao Min Yu Jin Zhou Chaowu Jin Yuanping Xu Xinxing Guo Yunzhi Wang Modeling and control of helicopter flight control system with a controllable Semi-rotary fluid viscous damper Alexandria Engineering Journal Fuzzy PID Variable universe APSO Fluid damper Parametric modeling |
| title | Modeling and control of helicopter flight control system with a controllable Semi-rotary fluid viscous damper |
| title_full | Modeling and control of helicopter flight control system with a controllable Semi-rotary fluid viscous damper |
| title_fullStr | Modeling and control of helicopter flight control system with a controllable Semi-rotary fluid viscous damper |
| title_full_unstemmed | Modeling and control of helicopter flight control system with a controllable Semi-rotary fluid viscous damper |
| title_short | Modeling and control of helicopter flight control system with a controllable Semi-rotary fluid viscous damper |
| title_sort | modeling and control of helicopter flight control system with a controllable semi rotary fluid viscous damper |
| topic | Fuzzy PID Variable universe APSO Fluid damper Parametric modeling |
| url | http://www.sciencedirect.com/science/article/pii/S1110016822004161 |
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