Power Supply Redundancy Design of Aircraft's Electric Braking Electro-Mechanical Actuation System
In this paper, a power source redundancy-optimization approach for aircraft electrical brake electromechanical actuation system was proposed. The PWM plus phase-shift (PPS) control method was introduced in Dual active half bridge, which limited the amplitude of transform's leakage inductance cu...
| Format: | Article |
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| Language: | zho |
| Published: |
EDP Sciences
2018-02-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/pdf/2018/01/jnwpu2018361p110.pdf |