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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2019
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Article
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Tab 5
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Research Article
Integrated Guidance and Control for Hypersonic Morphing Missile Based on Variable Span Auxiliary Control
Table 5
Results of the adaptive dynamic surface IGC method.
Terms
Va_span
Inva_span
30.86
43.21
60.47
57.63
2617
2518
45.05
46.33
3978
3660
6.1843
9.9400
0.1269
0.0880
0.0605
0.0579