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.

TermsVa_spanInva_span

30.8643.21
60.4757.63
26172518
45.0546.33
39783660
6.18439.9400
0.12690.0880
0.06050.0579