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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2020
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Article
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Fig 6
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Research Article
Disturbance Observer-Based Adaptive Control of Hypersonic Vehicles with Constrained Actuators
Figure 6
CDA and CDA rate in the comparison simulation: (a) canard deflection angle; (b) canard deflection angle rate.
(a)
(b)