Design of Three Dimensional Sliding Mode Terminal Guidance Law Based on Finite-Time and Small-Overshoot Prescribed Performance Control
In order to intercept a high-speed maneuvering target at a specific attack angle, a three dimensional sliding mode terminal guidance law is designed based on finite-time and small-overshoot prescribed performance control, which is a new method in control field. The linear sliding surface is designed...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Aero Weaponry
2023-04-01
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| Series: | Hangkong bingqi |
| Subjects: | |
| Online Access: | https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2022-00102.pdf |