Study on landing control method based on incremental dynamic inverse
Accurate landing control and improving the safety and reliability of the landing process are difficult issues in the safe recovery of carrier based aircraft. A landing control system based on incremental dynamic inverse is proposed. The method of an angle of attack maintenance loop and a trajectory...
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| Format: | Article |
| Language: | zho |
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Editorial Department of Advances in Aeronautical Science and Engineering
2024-12-01
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| Series: | Hangkong gongcheng jinzhan |
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| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2024101 |
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| _version_ | 1846091454827462656 |
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| author | DUAN Zhuoyi ZHAO Letian ZHANG Junhong LIU Xiaoxiong |
| author_facet | DUAN Zhuoyi ZHAO Letian ZHANG Junhong LIU Xiaoxiong |
| author_sort | DUAN Zhuoyi |
| collection | DOAJ |
| description | Accurate landing control and improving the safety and reliability of the landing process are difficult issues in the safe recovery of carrier based aircraft. A landing control system based on incremental dynamic inverse is proposed. The method of an angle of attack maintenance loop and a trajectory rate control loop based on incremental dynamic inversion is used，which can achieve decoupling of angle of attack and trajectory，as well as direct control of trajectory by direct lift. A differential tracker is introduced to estimate the track angular acceleration signal required in the incremental dynamic inverse control law. The landing control system is verified with simulation. The results show that the designed landing control system based on incremental dynamic inverse has excellent control accuracy，speed，and robustness. It can achieve accurate tracking of the trajectory under different sea conditions interference，and the landing points can meet the quality requirements for the distribution of carrier based aircraft landing points. |
| format | Article |
| id | doaj-art-ab5e7bf0aae84d7ebc0f21afd5ef73a8 |
| institution | Kabale University |
| issn | 1674-8190 |
| language | zho |
| publishDate | 2024-12-01 |
| publisher | Editorial Department of Advances in Aeronautical Science and Engineering |
| record_format | Article |
| series | Hangkong gongcheng jinzhan |
| spelling | doaj-art-ab5e7bf0aae84d7ebc0f21afd5ef73a82025-01-10T06:25:15ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902024-12-0115614314910.16615/j.cnki.1674-8190.2024.06.1210.16615/j.cnki.1674-8190.2024.06.12Study on landing control method based on incremental dynamic inverseDUAN Zhuoyi0ZHAO Letian1ZHANG Junhong2LIU Xiaoxiong3Overall Aerodynamic Design and Research Institute, AVIC The First Aircraft Institute, Xi'an 710089, ChinaFlight Control System Design and Research Institute, AVIC The First Aircraft Institute, Xi'an 710089, ChinaFlight Control System Design and Research Institute, AVIC The First Aircraft Institute, Xi'an 710089, ChinaSchool of Automation, Northwestern Polytechnical University, Xi'an 710129Accurate landing control and improving the safety and reliability of the landing process are difficult issues in the safe recovery of carrier based aircraft. A landing control system based on incremental dynamic inverse is proposed. The method of an angle of attack maintenance loop and a trajectory rate control loop based on incremental dynamic inversion is used，which can achieve decoupling of angle of attack and trajectory，as well as direct control of trajectory by direct lift. A differential tracker is introduced to estimate the track angular acceleration signal required in the incremental dynamic inverse control law. The landing control system is verified with simulation. The results show that the designed landing control system based on incremental dynamic inverse has excellent control accuracy，speed，and robustness. It can achieve accurate tracking of the trajectory under different sea conditions interference，and the landing points can meet the quality requirements for the distribution of carrier based aircraft landing points.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2024101carrier air wakeincremental dynamic inverse"magic carpet"landing control |
| spellingShingle | DUAN Zhuoyi ZHAO Letian ZHANG Junhong LIU Xiaoxiong Study on landing control method based on incremental dynamic inverse Hangkong gongcheng jinzhan carrier air wake incremental dynamic inverse "magic carpet" landing control |
| title | Study on landing control method based on incremental dynamic inverse |
| title_full | Study on landing control method based on incremental dynamic inverse |
| title_fullStr | Study on landing control method based on incremental dynamic inverse |
| title_full_unstemmed | Study on landing control method based on incremental dynamic inverse |
| title_short | Study on landing control method based on incremental dynamic inverse |
| title_sort | study on landing control method based on incremental dynamic inverse |
| topic | carrier air wake incremental dynamic inverse "magic carpet" landing control |
| url | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2024101 |
| work_keys_str_mv | AT duanzhuoyi studyonlandingcontrolmethodbasedonincrementaldynamicinverse AT zhaoletian studyonlandingcontrolmethodbasedonincrementaldynamicinverse AT zhangjunhong studyonlandingcontrolmethodbasedonincrementaldynamicinverse AT liuxiaoxiong studyonlandingcontrolmethodbasedonincrementaldynamicinverse |