Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints
文献类型：期刊论文
| 作者 | Hui-Bo Zhou1,2; Jun-Hong Song1; Shen-Min Song1 |
| 刊名 | International Journal of Automation and Computing
 |
| 出版日期 | 2018 |
| 卷号 | 15期号:2页码:218-227 |
| 关键词 | Autopilot impact angle nonsingular terminal sliding mode finite-time convergent guidance. |
| ISSN号 | 1476-8186 |
| DOI | 10.1007/s11633-016-0953-y |
| 英文摘要 | In order to improve the precision of guidance for the missile intercepting maneuvering targets, this paper proposes a sliding mode guidance law with impact angle constraints based on the equation of the relative motion of the missile and the target in a 2D plane. Two finite-time convergent guidance laws are proposed based on the nonsingular terminal sliding mode, while, two exponential convergent guidance laws involving dynamic delay are developed through applying the higher-order nonsingular terminal sliding mode. The simulations denote that, in all the four scenarios of the target0s maneuvering, the guidance laws are able to inhibit the chattering phenomenon of the sliding modes effectively; and from an expected aspect angle, the missiles could attack the targets with high precision and fast speed. |
| 源URL | [http://ir.ia.ac.cn/handle/173211/42404]  |
| 专题 | 自动化研究所_学术期刊_International Journal of Automation and Computing |
| 作者单位 | 1.Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China 2.School of Mathematical Sciences, Harbin Normal University, Harbin 150009, China |
| 推荐引用方式 GB/T 7714 | Hui-Bo Zhou,Jun-Hong Song,Shen-Min Song. Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints[J]. International Journal of Automation and Computing,2018,15(2):218-227. |
| APA | Hui-Bo Zhou,Jun-Hong Song,&Shen-Min Song.(2018).Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints.International Journal of Automation and Computing,15(2),218-227. |
| MLA | Hui-Bo Zhou,et al."Sliding Mode Guidance Law Considering Missile Dynamic Characteristics and Impact Angle Constraints".International Journal of Automation and Computing 15.2(2018):218-227. |
入库方式： OAI收割
来源：自动化研究所
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