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Journal of Electrical and Computer Engineering
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Journal of Electrical and Computer Engineering
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2017
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Article
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Fig 15
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Research Article
Research on HILS Technology Applied on Aircraft Electric Braking System
Figure 15
HILS results when deceleration rate is 2.1.
(a)
Running distance
(b)
Aircraft speed
(c)
Wheel speed
(d)
Actual brake pressure
(e)
Given brake pressure