Fly-by-Wire Actuation System Modeling and Force Fight Equalization Research
Aiming at the actuation system force fight problem resulted from active-active operational mode of fly-by-wire aircraft, and considering the technical maturity and reliability from safety aspect, the inertial integration algorithm and PI control law are established. After tradeoff study on these two...
| Format: | Article |
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| Language: | zho |
| Published: |
The Northwestern Polytechnical University
2020-06-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2020/03/jnwpu2020383p643/jnwpu2020383p643.html |