| 采用直接力的空空导弹越肩发射控制设计 |
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| 引用本文： | 闫亮,马克茂,董继鹏,张金鹏.采用直接力的空空导弹越肩发射控制设计[J].航空兵器,2013(6):3-8. |
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| 作者姓名： | 闫亮 马克茂 董继鹏 张金鹏 |
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| 作者单位： | [1]哈尔滨工业大学航天学院,哈尔滨150001 [2]中国空空导弹研究院,河南洛阳471009 |
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| 基金项目： | 国家自然科学基金（61174001）;航空科学基金（20120177005） |
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| 摘 要： | 针对空空导弹越肩发射的姿态控制需求，采用直接力控制装置，分别建立了小攻角模型和大攻角模型，利用滑模变结构控制方法设计了姿态控制律，所设计的控制律能够满足导弹越肩发射快速转弯的要求，仿真结果说明了此方法的有效性。
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| 关 键 词： | 空空导弹 越肩发射 直接力装置 气动力参数 姿态控制 滑模控制 |
Design of Over-the-Shoulder Launch Control for Air-to-Air Missiles with Lateral Jets |
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| YAN Liang,MA Ke-mao,DONG Ji-peng,ZHANG Jin-peng.Design of Over-the-Shoulder Launch Control for Air-to-Air Missiles with Lateral Jets[J].Aero Weaponry,2013(6):3-8. |
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| Authors: | YAN Liang MA Ke-mao DONG Ji-peng ZHANG Jin-peng |
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| Affiliation: | 1. School of Astronautics, Harbin Institute of Technology, Harbin 150001, China; 2. China Airborne Missile Academy, Luoyang 471009, China) |
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| Abstract: | To satisfy the attitude control demands in the over-the-shoulder launch of air-to-air mis- siles, lateral jets are adopted. Mathematical models covering small and large angle of attack ranges are constructed respectively. Attitude control laws are designed based on sliding mode control. The proposed control laws satisfies the high turning rate requirment in the over-the-shoulder launch, and the simulation results show the effectiveness of the design. |
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| Keywords: | air-to-air missiles over-the-shoulder launch lateral thrust set aerodynamic coeffi-cients attitude control sliding mode control |
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