Design of EKV Sliding Mode Guidance Law Based on Terminal Angle Limit
A guidance method based on terminal angle limit was researched. By deduction, the relationship between target velocity direction and LOS angle velocity was found in LOS coordinate system, and intercept model based on terminal angle limit was built. Furthermore, on the basis of model nonlinearity, th...
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| Veröffentlicht in: | Danjian yu Zhidao Xuebao / Journal of Projectiles, Rockets, Missiles and Guidance Rockets, Missiles and Guidance, 2015-10, Vol.35 (5), p.22-29 |
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| container_end_page | 29 |
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| container_issue | 5 |
| container_start_page | 22 |
| container_title | Danjian yu Zhidao Xuebao / Journal of Projectiles, Rockets, Missiles and Guidance |
| container_volume | 35 |
| creator | Nie, Chuang Shu, Jiansheng Meng, Shaofei |
| description | A guidance method based on terminal angle limit was researched. By deduction, the relationship between target velocity direction and LOS angle velocity was found in LOS coordinate system, and intercept model based on terminal angle limit was built. Furthermore, on the basis of model nonlinearity, the double ring sliding mode guidance law was designed and sliding mode approach rate was also chosen reasonably. The simulation result explained the effect of this method could reduce attack angle and target-missing quality, the aim of direct rail or reverse course interceptor effectively was targeted. |
| doi_str_mv | 10.15892/j.cnki.djzdxb.2015.05.006 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 1673-9728 |
| ispartof | Danjian yu Zhidao Xuebao / Journal of Projectiles, Rockets, Missiles and Guidance, 2015-10, Vol.35 (5), p.22-29 |
| issn | 1673-9728 |
| language | chi |
| recordid | cdi_proquest_miscellaneous_1778070526 |
| source | Alma/SFX Local Collection |
| subjects | Computer simulation Design engineering Guidance (motion) Missiles Nonlinearity Rockets Sliding mode Terminals |
| title | Design of EKV Sliding Mode Guidance Law Based on Terminal Angle Limit |
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