| 变后掠翼舰载机抗侧风自动着舰引导系统 |
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| 引用本文： | 郑峰婴,杨一栋.变后掠翼舰载机抗侧风自动着舰引导系统[J].飞行力学,2011,29(2):37-40. |
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| 作者姓名： | 郑峰婴 杨一栋 |
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| 作者单位： | 1. 南京航空航天大学高新技术研究院,江苏,南京,210016
2. 南京航空航天大学自动化学院,江苏,南京,210016 |
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| 基金项目： | 南京航空航天大学青年科研基金(Y0835-GXY) |
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| 摘 要： | 舰载机在航母上降落时,舰尾气流的扰动是影响着舰精度的主要因素.以变后掠翼舰载机为研究对象,根据其操纵特性,设计了引人侧偏速率反馈的抗侧风飞控系统控制律,优化自动着舰引导系统轨迹控制器系统参数,并根据系统结构配置构建仿真系统.通过对比侧偏速率反馈引人前后的系统性能表明,引人侧偏速率反馈明显降低了舰尾流对变后掠翼舰载机的影...
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| 关 键 词： | 抗侧风 变后掠翼 舰载机 自动着舰 |
Counteracting side wind in automatic carrier landing system for variable swept wing carrier-aircraft |
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| MENG Feng-ying,YANG Yi-dong.Counteracting side wind in automatic carrier landing system for variable swept wing carrier-aircraft[J].Flight Dynamics,2011,29(2):37-40. |
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| Authors: | MENG Feng-ying YANG Yi-dong |
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| Institution: | ZHENG Feng-ying1,YANG Yi-dong2(1.Academy of Frontier Science,NUAA,Nanjing 210016,China,2.College of Automation,China) |
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| Abstract: | Wind and atmosphere turbulence have deep influence on landing precision,when the aircraft is preparing to land on the carrier.The variable swept wing carrier-aircraft was regarded as research object,and the flight control law introduced side velocity feedback was developed with its handling feature.Trajectory control parameter of the automatic carrier landing system was optimized.The simulation system was constructed for verifying and evaluating the performance of this system.The simulation result indicates... |
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| Keywords: | counteracting side wind variable swept wing carrier-aircraft automatic carrier landing |
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