Cooperative control method of multi-missile formation under uncontrollable speed
Under the missile speed is uncontrollable, a design method of multi-missile formation flight controller based on the sliding mode variable structure control theory and adaptive dynamic surface control theory is proposed. Firstly, according to the relative position of the leader and the follower in t...
| Format: | Article |
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| Language: | zho |
| Published: |
The Northwestern Polytechnical University
2021-04-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2021/02/jnwpu2021392p249/jnwpu2021392p249.html |