Multicriteria Optimization via Parameter Space Investigation for Ultralow-Altitude Airdrop L1 Adaptive Controller
This paper presents preliminary results of the application of the parameter space investigation method for the design of the L1 flight control system implemented on the ultralow-altitude airdrop process. In particular, the study has established the task performance level of airdrop mission which is...
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Published in | International journal of aeronautical and space sciences Vol. 21; no. 1; pp. 224 - 238 |
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Main Authors | , , , |
Format | Journal Article |
Language | English |
Published |
Seoul
The Korean Society for Aeronautical & Space Sciences (KSAS)
01.03.2020
한국항공우주학회 |
Subjects | |
Online Access | Get full text |
ISSN | 2093-274X 2093-2480 |
DOI | 10.1007/s42405-019-00199-w |
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Abstract | This paper presents preliminary results of the application of the parameter space investigation method for the design of the L1 flight control system implemented on the ultralow-altitude airdrop process. In particular, the study has established the task performance level of airdrop mission which is chosen as the optimization objective in this paper. According to the characteristics of ultralow-altitude airdrop process, 12 optimization criteria are designated as the constraints during the multicriteria optimization. After two iterations, the task performance level of the airdrop is improved from “Moderate” to “Expected”. The results in the paper confirms the suitability of the parameter space investigation method for the multicriteria design optimization of an airdrop flight control system subject to desired control specifications. In addition, the robustness and dynamic response of the flight control system are significantly improved after optimization. Moreover, the analysis of optimization results has contributed to a deeper understanding of the relationship between L1 controller parameters and airdrop task performance. |
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AbstractList | This paper presents preliminary results of the application of the parameter space investigation method for the design of the L1 flight control system implemented on the ultralow-altitude airdrop process. In particular, the study has established the task performance level of airdrop mission which is chosen as the optimization objective in this paper. According to the characteristics of ultralow-altitude airdrop process, 12 optimization criteria are designated as the constraints during the multicriteria optimization. After two iterations, the task performance level of the airdrop is improved from “Moderate” to “Expected”. The results in the paper confirms the suitability of the parameter space investigation method for the multicriteria design optimization of an airdrop flight control system subject to desired control specifications. In addition, the robustness and dynamic response of the flight control system are significantly improved after optimization. Moreover, the analysis of optimization results has contributed to a deeper understanding of the relationship between L1 controller parameters and airdrop task performance. This paper presents preliminary results of the application of the parameter space investigation method for the design of the L1 flight control system implemented on the ultralow-altitude airdrop process. In particular, the study has established the task performance level of airdrop mission which is chosen as the optimization objective in this paper. According to the characteristics of ultralow-altitude airdrop process, 12 optimization criteria are designated as the constraints during the multicriteria optimization. After two iterations, the task performance level of the airdrop is improved from “Moderate” to “Expected”. The results in the paper confirms the suitability of the parameter space investigation method for the multicriteria design optimization of an airdrop flight control system subject to desired control specifications. In addition, the robustness and dynamic response of the flight control system are significantly improved after optimization. Moreover, the analysis of optimization results has contributed to a deeper understanding of the relationship between L1 controller parameters and airdrop task performance. KCI Citation Count: 0 |
Author | Liu, Ri Zhu, Peng Dong, Wenhan Mao, Yuhao |
Author_xml | – sequence: 1 givenname: Peng surname: Zhu fullname: Zhu, Peng organization: Aeronautics Engineering College, Air Force Engineering University – sequence: 2 givenname: Wenhan surname: Dong fullname: Dong, Wenhan email: dongwenhan@sina.com organization: Aeronautics Engineering College, Air Force Engineering University – sequence: 3 givenname: Yuhao surname: Mao fullname: Mao, Yuhao organization: Aeronautics Engineering College, Air Force Engineering University – sequence: 4 givenname: Ri surname: Liu fullname: Liu, Ri organization: Theory Training Department, Air Force Harbin Flight Academy |
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Cites_doi | 10.2514/1.47996 10.1109/TAC.2007.914282 10.1016/j.cja.2015.02.008 10.1109/TSMC.2016.2558098 10.1016/j.automatica.2014.10.015 10.1007/s12555-017-0014-5 10.2514/1.G000566 10.1007/s00158-003-0368-6 10.1007/978-94-015-9968-9 10.1002/acs.2419 10.2514/6.2010-7691 |
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Keywords | Parameter space investigation Ultralow-altitude airdrop L1-adaptive control Parameter optimization |
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References | Kharisov, Hovakimyan, Åström (CR5) 2014; 28 Marler, Arora (CR20) 2004; 26 Statnikov, Matusov (CR18) 2002 Sobol, Statnikov (CR19) 2006 Cao, Hovakimyan (CR8) 2006; 53 Chang, Zhu, Liu, Dong (CR12) 2018; 16 CR17 CR9 Xu (CR3) 2016; 47 CR14 Xu, Chen (CR1) 2016; 13 CR13 Liu, Sun, Dong (CR2) 2015; 28 Gang (CR7) 2014; 50 CR21 Jafarnejadsani, Sun, Lee, Hovakimyan (CR15) 2017; 40 Hovakimyan, Cao (CR16) 2010 Liu, Sun, Dong (CR10) 2015; 2015 Liu, Tao, Joshi (CR4) 2010; 33 Wenhan, Xiuxia, Yan (CR6) 2010; 32 Xiuxia, Yungang, Wenhan, Ri (CR11) 2015; 32 B Xu (199_CR3) 2016; 47 199_CR13 E Kharisov (199_CR5) 2014; 28 D Wenhan (199_CR6) 2010; 32 T Gang (199_CR7) 2014; 50 199_CR21 R Liu (199_CR2) 2015; 28 Y Liu (199_CR4) 2010; 33 H Jafarnejadsani (199_CR15) 2017; 40 S Xiuxia (199_CR11) 2015; 32 IM Sobol (199_CR19) 2006 J Chang (199_CR12) 2018; 16 N Hovakimyan (199_CR16) 2010 RB Statnikov (199_CR18) 2002 B Xu (199_CR1) 2016; 13 199_CR17 199_CR9 RT Marler (199_CR20) 2004; 26 C Cao (199_CR8) 2006; 53 199_CR14 R Liu (199_CR10) 2015; 2015 |
References_xml | – ident: CR21 – volume: 32 start-page: 1485 issue: 7 year: 2010 end-page: 1488 ident: CR6 article-title: Backstepping model reference robust controller design for flight control publication-title: Syst Eng Electron – year: 2006 ident: CR19 publication-title: Selecting optimal parameters in multicriteria problems – volume: 13 start-page: 1 issue: 2 year: 2016 end-page: 8 ident: CR1 article-title: Review of modeling and control during transport airdrop process publication-title: Int J Adv Robot Syst – ident: CR14 – volume: 32 start-page: 598 issue: 5 year: 2015 end-page: 606 ident: CR11 article-title: Design of longitudinal controller for flight in heavy-weight airdrop based on optimal control and L1 adaptive publication-title: Control Theory Appl – ident: CR17 – ident: CR13 – volume: 33 start-page: 1500 issue: 5 year: 2010 end-page: 1517 ident: CR4 article-title: Modeling and model reference adaptive control of aircraft with asymmetric damage publication-title: J Guid Control Dyn doi: 10.2514/1.47996 – volume: 53 start-page: 586 issue: 2 year: 2006 end-page: 591 ident: CR8 article-title: Design and analysis of a novel L1 adaptive control architecture with guaranteed transient performance publication-title: IEEE Trans Autom Control doi: 10.1109/TAC.2007.914282 – ident: CR9 – start-page: 2010 year: 2010 ident: CR16 publication-title: L1 adaptive control theory – volume: 28 start-page: 478 issue: 2 year: 2015 end-page: 487 ident: CR2 article-title: Dynamics modeling and control of a transport aircraft for ultra-low altitude airdrop publication-title: Chin J Aeronaut doi: 10.1016/j.cja.2015.02.008 – volume: 47 start-page: 161 issue: 1 year: 2016 end-page: 170 ident: CR3 article-title: Disturbance observer based dynamic surface control of transport aircraft with continuous heavy cargo airdrop publication-title: IEEE Trans Syst Man Cybern Syst doi: 10.1109/TSMC.2016.2558098 – volume: 2015 start-page: 1 issue: 11 year: 2015 end-page: 15 ident: CR10 article-title: Dynamics modeling and L1 adaptive control of a transport aircraft for heavy weight airdrop publication-title: Math Probl Eng – volume: 50 start-page: 2737 issue: 11 year: 2014 end-page: 2764 ident: CR7 article-title: Multivariable adaptive control: a survey publication-title: Automatica doi: 10.1016/j.automatica.2014.10.015 – volume: 16 start-page: 461 year: 2018 ident: CR12 article-title: Lateral control for ultra-low altitude airdrop based on the L1 adaptive control augmentation publication-title: Int J Control Autom Syst doi: 10.1007/s12555-017-0014-5 – volume: 40 start-page: 1 year: 2017 end-page: 13 ident: CR15 article-title: Optimized L1 adaptive controller for trajectory tracking of an indoor quadrotor publication-title: J Guid Control Dyn doi: 10.2514/1.G000566 – volume: 26 start-page: 369 issue: 6 year: 2004 end-page: 395 ident: CR20 article-title: Survey of multi-objective optimization methods for engineering publication-title: Struct Multidiscip Optim doi: 10.1007/s00158-003-0368-6 – year: 2002 ident: CR18 publication-title: Multicriteria analysis in engineering doi: 10.1007/978-94-015-9968-9 – volume: 28 start-page: 633 issue: 7 year: 2014 end-page: 663 ident: CR5 article-title: Comparison of architectures and robustness of model reference adaptive controllers and L1 adaptive controllers publication-title: Int J Adapt Control Signal Process doi: 10.1002/acs.2419 – volume: 47 start-page: 161 issue: 1 year: 2016 ident: 199_CR3 publication-title: IEEE Trans Syst Man Cybern Syst doi: 10.1109/TSMC.2016.2558098 – volume: 50 start-page: 2737 issue: 11 year: 2014 ident: 199_CR7 publication-title: Automatica doi: 10.1016/j.automatica.2014.10.015 – volume: 53 start-page: 586 issue: 2 year: 2006 ident: 199_CR8 publication-title: IEEE Trans Autom Control doi: 10.1109/TAC.2007.914282 – volume: 2015 start-page: 1 issue: 11 year: 2015 ident: 199_CR10 publication-title: Math Probl Eng – volume-title: Multicriteria analysis in engineering year: 2002 ident: 199_CR18 doi: 10.1007/978-94-015-9968-9 – volume: 13 start-page: 1 issue: 2 year: 2016 ident: 199_CR1 publication-title: Int J Adv Robot Syst – volume: 28 start-page: 478 issue: 2 year: 2015 ident: 199_CR2 publication-title: Chin J Aeronaut doi: 10.1016/j.cja.2015.02.008 – volume: 28 start-page: 633 issue: 7 year: 2014 ident: 199_CR5 publication-title: Int J Adapt Control Signal Process doi: 10.1002/acs.2419 – volume-title: Selecting optimal parameters in multicriteria problems year: 2006 ident: 199_CR19 – ident: 199_CR21 – volume: 33 start-page: 1500 issue: 5 year: 2010 ident: 199_CR4 publication-title: J Guid Control Dyn doi: 10.2514/1.47996 – ident: 199_CR9 – volume: 32 start-page: 598 issue: 5 year: 2015 ident: 199_CR11 publication-title: Control Theory Appl – volume: 16 start-page: 461 year: 2018 ident: 199_CR12 publication-title: Int J Control Autom Syst doi: 10.1007/s12555-017-0014-5 – volume: 26 start-page: 369 issue: 6 year: 2004 ident: 199_CR20 publication-title: Struct Multidiscip Optim doi: 10.1007/s00158-003-0368-6 – ident: 199_CR17 doi: 10.2514/6.2010-7691 – start-page: 2010 volume-title: L1 adaptive control theory year: 2010 ident: 199_CR16 – ident: 199_CR14 – ident: 199_CR13 – volume: 32 start-page: 1485 issue: 7 year: 2010 ident: 199_CR6 publication-title: Syst Eng Electron – volume: 40 start-page: 1 year: 2017 ident: 199_CR15 publication-title: J Guid Control Dyn doi: 10.2514/1.G000566 |
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SubjectTerms | Aerospace Technology and Astronautics Engineering Fluid- and Aerodynamics Original Paper 항공우주공학 |
Title | Multicriteria Optimization via Parameter Space Investigation for Ultralow-Altitude Airdrop L1 Adaptive Controller |
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