Study on the Aircraft Taxiing Control during Ground Operations Based on the Rate of Nosewheel Deflection
To realize the aircraft maneuvering turn during ground operations, the aircraft’s nosewheel control system should provide the rate of nosewheel deflection as higher as possible. To prevent the aircraft’s wheel from lateral slip the deflection rate should be limited in a certain range. Take a certain...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | zho |
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Editorial Department of Advances in Aeronautical Science and Engineering
2019-04-01
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| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2019028?st=article_issue |
| _version_ | 1828130357240659968 |
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| author | Lu Sheng Zhong Xiaohong Huang Zhijun Pei Huaping |
| author_facet | Lu Sheng Zhong Xiaohong Huang Zhijun Pei Huaping |
| author_sort | Lu Sheng |
| collection | DOAJ |
| description | To realize the aircraft maneuvering turn during ground operations, the aircraft’s nosewheel control system should provide the rate of nosewheel deflection as higher as possible. To prevent the aircraft’s wheel from lateral slip the deflection rate should be limited in a certain range. Take a certain type of aircraft as an example, the effect of lateral slip under the large nosewheel deflection, the friction coefficient on the ground, the aircraft taxiing speed and the rate of nose wheel deflection are analyzed. Results show that the aircraft makes large nosewheel deflection at the rate of 0.3~0.4 rad/s, it can basically meet the ground stability requirements, but to reduce the risk of lateral slip on the low friction pavement, the rate of nosewheel deflection needs to be reduced when the nose wheel deflects to a large angle. |
| first_indexed | 2024-04-11T16:31:48Z |
| format | Article |
| id | doaj.art-c1b9405e09c242b792d02add71bbe884 |
| institution | Directory Open Access Journal |
| issn | 1674-8190 |
| language | zho |
| last_indexed | 2024-04-11T16:31:48Z |
| publishDate | 2019-04-01 |
| publisher | Editorial Department of Advances in Aeronautical Science and Engineering |
| record_format | Article |
| series | Hangkong gongcheng jinzhan |
| spelling | doaj.art-c1b9405e09c242b792d02add71bbe8842022-12-22T04:13:59ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902019-04-0110228328810.16615/j.cnki.1674-8190.2019.02.02020190220Study on the Aircraft Taxiing Control during Ground Operations Based on the Rate of Nosewheel DeflectionLu Sheng0Zhong Xiaohong1Huang Zhijun2Pei Huaping3Aircraft Design Institute, Jiangxi Hongdu Aviation Industry Group Co., Ltd., Nanchang 330024, ChinaAircraft Design Institute, Jiangxi Hongdu Aviation Industry Group Co., Ltd., Nanchang 330024, ChinaAircraft Design Institute, Jiangxi Hongdu Aviation Industry Group Co., Ltd., Nanchang 330024, ChinaAircraft Design Institute, Jiangxi Hongdu Aviation Industry Group Co., Ltd., Nanchang 330024, ChinaTo realize the aircraft maneuvering turn during ground operations, the aircraft’s nosewheel control system should provide the rate of nosewheel deflection as higher as possible. To prevent the aircraft’s wheel from lateral slip the deflection rate should be limited in a certain range. Take a certain type of aircraft as an example, the effect of lateral slip under the large nosewheel deflection, the friction coefficient on the ground, the aircraft taxiing speed and the rate of nose wheel deflection are analyzed. Results show that the aircraft makes large nosewheel deflection at the rate of 0.3~0.4 rad/s, it can basically meet the ground stability requirements, but to reduce the risk of lateral slip on the low friction pavement, the rate of nosewheel deflection needs to be reduced when the nose wheel deflects to a large angle.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2019028?st=article_issuethe rate of nosewheel deflectionthe large nosewheel deflectionthe lateral slip |
| spellingShingle | Lu Sheng Zhong Xiaohong Huang Zhijun Pei Huaping Study on the Aircraft Taxiing Control during Ground Operations Based on the Rate of Nosewheel Deflection Hangkong gongcheng jinzhan the rate of nosewheel deflection the large nosewheel deflection the lateral slip |
| title | Study on the Aircraft Taxiing Control during Ground Operations Based on the Rate of Nosewheel Deflection |
| title_full | Study on the Aircraft Taxiing Control during Ground Operations Based on the Rate of Nosewheel Deflection |
| title_fullStr | Study on the Aircraft Taxiing Control during Ground Operations Based on the Rate of Nosewheel Deflection |
| title_full_unstemmed | Study on the Aircraft Taxiing Control during Ground Operations Based on the Rate of Nosewheel Deflection |
| title_short | Study on the Aircraft Taxiing Control during Ground Operations Based on the Rate of Nosewheel Deflection |
| title_sort | study on the aircraft taxiing control during ground operations based on the rate of nosewheel deflection |
| topic | the rate of nosewheel deflection the large nosewheel deflection the lateral slip |
| url | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2019028?st=article_issue |
| work_keys_str_mv | AT lusheng studyontheaircrafttaxiingcontrolduringgroundoperationsbasedontherateofnosewheeldeflection AT zhongxiaohong studyontheaircrafttaxiingcontrolduringgroundoperationsbasedontherateofnosewheeldeflection AT huangzhijun studyontheaircrafttaxiingcontrolduringgroundoperationsbasedontherateofnosewheeldeflection AT peihuaping studyontheaircrafttaxiingcontrolduringgroundoperationsbasedontherateofnosewheeldeflection |