Optimal Design of the Pitching Mechanism Considering the Influence of Erecting Angle Curves
The erecting angle curve directly affects the angle acceleration of the pitching mechanism of the rocket, and then directly affects the instantaneous thrust and instantaneous power of the pitching mechanism, ultimately affects the best arrangement of the pitching mechanism. As the requirements of th...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Journal of Mechanical Transmission
2024-12-01
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| Series: | Jixie chuandong |
| Subjects: | |
| Online Access: | http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2024.12.018 |
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| author | Yuan Yi Deng Wenzhu Wu Bude Wang Yuqi Lu Wei Ding Yuli |
| author_facet | Yuan Yi Deng Wenzhu Wu Bude Wang Yuqi Lu Wei Ding Yuli |
| author_sort | Yuan Yi |
| collection | DOAJ |
| description | The erecting angle curve directly affects the angle acceleration of the pitching mechanism of the rocket, and then directly affects the instantaneous thrust and instantaneous power of the pitching mechanism, ultimately affects the best arrangement of the pitching mechanism. As the requirements of the pitching mechanism for smooth start & stop and erecting time, the angular acceleration of the pitching mechanism can't be ignored, and the optimal design of the pitching mechanism considering the influence of the erecting angle curve was proposed. The key parameters of the erecting angle curve and its restrictions were analyzed, the influence of the vertical angle curve on the instantaneous thrust & power of the electric cylinder was analyzed, the mathematical mode for the optimization of the pitching mechanism considering the influence of erecting angle curve was established, and the optimal pitch mechanism layout and the erecting angle curve were obtained by using the fmincon function based on the sequential quadratic programming (SQP) algorithm in Matlab sofware. Erecting test results of a rocket launcher show that the optimal design of the pitching mechanism considering the influence of the erecting angle curve can effectively reduce the maximum power of the electric pushrod, rather than reduce the maximum thrust of the electric pushrod. |
| format | Article |
| id | doaj-art-1dc3c29f00d449ab9ae6b53c2d79f459 |
| institution | Kabale University |
| issn | 1004-2539 |
| language | zho |
| publishDate | 2024-12-01 |
| publisher | Editorial Office of Journal of Mechanical Transmission |
| record_format | Article |
| series | Jixie chuandong |
| spelling | doaj-art-1dc3c29f00d449ab9ae6b53c2d79f4592025-01-10T15:02:27ZzhoEditorial Office of Journal of Mechanical TransmissionJixie chuandong1004-25392024-12-014812513078919313Optimal Design of the Pitching Mechanism Considering the Influence of Erecting Angle CurvesYuan YiDeng WenzhuWu BudeWang YuqiLu WeiDing YuliThe erecting angle curve directly affects the angle acceleration of the pitching mechanism of the rocket, and then directly affects the instantaneous thrust and instantaneous power of the pitching mechanism, ultimately affects the best arrangement of the pitching mechanism. As the requirements of the pitching mechanism for smooth start & stop and erecting time, the angular acceleration of the pitching mechanism can't be ignored, and the optimal design of the pitching mechanism considering the influence of the erecting angle curve was proposed. The key parameters of the erecting angle curve and its restrictions were analyzed, the influence of the vertical angle curve on the instantaneous thrust & power of the electric cylinder was analyzed, the mathematical mode for the optimization of the pitching mechanism considering the influence of erecting angle curve was established, and the optimal pitch mechanism layout and the erecting angle curve were obtained by using the fmincon function based on the sequential quadratic programming (SQP) algorithm in Matlab sofware. Erecting test results of a rocket launcher show that the optimal design of the pitching mechanism considering the influence of the erecting angle curve can effectively reduce the maximum power of the electric pushrod, rather than reduce the maximum thrust of the electric pushrod.http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2024.12.018Rocket launcherPitching mechanismErecting angle curveSQP algorithmFmincon function |
| spellingShingle | Yuan Yi Deng Wenzhu Wu Bude Wang Yuqi Lu Wei Ding Yuli Optimal Design of the Pitching Mechanism Considering the Influence of Erecting Angle Curves Jixie chuandong Rocket launcher Pitching mechanism Erecting angle curve SQP algorithm Fmincon function |
| title | Optimal Design of the Pitching Mechanism Considering the Influence of Erecting Angle Curves |
| title_full | Optimal Design of the Pitching Mechanism Considering the Influence of Erecting Angle Curves |
| title_fullStr | Optimal Design of the Pitching Mechanism Considering the Influence of Erecting Angle Curves |
| title_full_unstemmed | Optimal Design of the Pitching Mechanism Considering the Influence of Erecting Angle Curves |
| title_short | Optimal Design of the Pitching Mechanism Considering the Influence of Erecting Angle Curves |
| title_sort | optimal design of the pitching mechanism considering the influence of erecting angle curves |
| topic | Rocket launcher Pitching mechanism Erecting angle curve SQP algorithm Fmincon function |
| url | http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2024.12.018 |
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