Second-Order Sliding Mode Guidance Law considering Second-Order Dynamics of Autopilot
Aiming at the requirement that some missiles need to meet certain impact angles when attacking targets, we consider the second-order dynamic characteristics of autopilot, thereby proposing a second-order sliding mode guidance law with impact angle constraint. Firstly, based on the terminal sliding m...
Tallennettuna:
| Päätekijät: | , |
|---|---|
| Aineistotyyppi: | Artigo |
| Kieli: | Inglês |
| Julkaistu: |
Wiley
2019-01-01
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| Sarja: | Journal of Control Science and Engineering |
| Linkit: | http://dx.doi.org/10.1155/2019/8573140 |
| Tagit: |
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