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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2015
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Article
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Tab 2
/
Research Article
Designing Backstepping Control System for Hypersonic Vehicle Based on Feedback Linearization
Table 2
The influence of rudder deflection to velocity system.
0.3
ā20
45
3171
3216
0.3
20
84
3171
3255