Model Predictive Control for Automatic Carrier Landing with Time Delay
This paper focuses on the problem of automatic carrier landing control with time delay, and an antidelay model predictive control (AD-MPC) scheme for carrier landing based on the symplectic pseudospectral (SP) method and a prediction error method with particle swarm optimization (PE-PSO) is designed...
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| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2021-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2021/8613498 |
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| _version_ | 1832545969595482112 |
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| author | Kaikai Cui Wei Han Yujie Liu Xinwei Wang Xichao Su Jie Liu |
| author_facet | Kaikai Cui Wei Han Yujie Liu Xinwei Wang Xichao Su Jie Liu |
| author_sort | Kaikai Cui |
| collection | DOAJ |
| description | This paper focuses on the problem of automatic carrier landing control with time delay, and an antidelay model predictive control (AD-MPC) scheme for carrier landing based on the symplectic pseudospectral (SP) method and a prediction error method with particle swarm optimization (PE-PSO) is designed. Firstly, the mathematical model for carrier landing control with time delay is given, and based on the Padé approximation (PA) principle, the model with time delay is transformed into an equivalent nondelay one. Furthermore, a guidance trajectory based on the predicted trajectory shape and position deviation is designed in the MPC framework to eliminate the influence of carrier deck motion and real-time error. At the same time, a rolling optimal control block is designed based on the SP algorithm, in which the steady-state carrier air wake compensation is introduced to suppress the interference of the air wake. On this basis, the PE-PSO delay estimation algorithm is proposed to estimate the unknown delay parameter in the equivalent control model. The simulation results show that the delay estimation error of the PE-PSO algorithm is smaller than 2 ms, and the AD-MPC algorithm proposed in this paper can limit the landing height error within ±0.14 m under the condition of multiple disturbances and system input delay. The control accuracy of AD-MPC is much higher than that of the traditional pole assignment algorithm, and its computational efficiency meets the requirement of real-time online tracking. |
| format | Article |
| id | doaj-art-17e46546373e406dbc6278c781443ff5 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2021-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-17e46546373e406dbc6278c781443ff52025-02-03T07:24:11ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742021-01-01202110.1155/2021/86134988613498Model Predictive Control for Automatic Carrier Landing with Time DelayKaikai Cui0Wei Han1Yujie Liu2Xinwei Wang3Xichao Su4Jie Liu5Naval Aviation University, Yantai 264001, ChinaNaval Aviation University, Yantai 264001, ChinaNaval Aviation University, Yantai 264001, ChinaDepartment of Engineering Mechanics, State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, ChinaNaval Aviation University, Yantai 264001, ChinaWar Research Institute, Academy of Military Sciences, Beijing 100850, ChinaThis paper focuses on the problem of automatic carrier landing control with time delay, and an antidelay model predictive control (AD-MPC) scheme for carrier landing based on the symplectic pseudospectral (SP) method and a prediction error method with particle swarm optimization (PE-PSO) is designed. Firstly, the mathematical model for carrier landing control with time delay is given, and based on the Padé approximation (PA) principle, the model with time delay is transformed into an equivalent nondelay one. Furthermore, a guidance trajectory based on the predicted trajectory shape and position deviation is designed in the MPC framework to eliminate the influence of carrier deck motion and real-time error. At the same time, a rolling optimal control block is designed based on the SP algorithm, in which the steady-state carrier air wake compensation is introduced to suppress the interference of the air wake. On this basis, the PE-PSO delay estimation algorithm is proposed to estimate the unknown delay parameter in the equivalent control model. The simulation results show that the delay estimation error of the PE-PSO algorithm is smaller than 2 ms, and the AD-MPC algorithm proposed in this paper can limit the landing height error within ±0.14 m under the condition of multiple disturbances and system input delay. The control accuracy of AD-MPC is much higher than that of the traditional pole assignment algorithm, and its computational efficiency meets the requirement of real-time online tracking.http://dx.doi.org/10.1155/2021/8613498 |
| spellingShingle | Kaikai Cui Wei Han Yujie Liu Xinwei Wang Xichao Su Jie Liu Model Predictive Control for Automatic Carrier Landing with Time Delay International Journal of Aerospace Engineering |
| title | Model Predictive Control for Automatic Carrier Landing with Time Delay |
| title_full | Model Predictive Control for Automatic Carrier Landing with Time Delay |
| title_fullStr | Model Predictive Control for Automatic Carrier Landing with Time Delay |
| title_full_unstemmed | Model Predictive Control for Automatic Carrier Landing with Time Delay |
| title_short | Model Predictive Control for Automatic Carrier Landing with Time Delay |
| title_sort | model predictive control for automatic carrier landing with time delay |
| url | http://dx.doi.org/10.1155/2021/8613498 |
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