Research Article

Integrated Guidance and Control Method for the Interception of Maneuvering Hypersonic Vehicle Based on High Order Sliding Mode Approach

Table 2

Average miss distance of 50 simulations.

Target speedPNHOSM-IGC
()
HOSM-IGC
()

= 2000 m/s1.15 m0.860.73 m
= 3000 m/s2.61 m1.171.06
= 4000 m/s5.42 m1.561.34