Research Article

Integrated Guidance and Control for Hypersonic Morphing Missile Based on Variable Span Auxiliary Control

Table 1

Missile characteristic parameter.

NameValueNameValueNameValue

3.43 m0.92 m
8.00 m1.63 m
4.70 m2.55 m5.66 m
9.73 m1.70 m1.148 m
1.14 m0.85 m0.766 m
2.12 m0.91 m5000 kg
100 kg15064 kg·m2150646 kg·m2