Research Article
Integrated Guidance and Control Method for the Interception of Maneuvering Hypersonic Vehicle Based on High Order Sliding Mode Approach
Table 1
Initial conditions.
| | Variable | Description | Value |
| | (, ) | Missile initial position | (0 km, 18 km) | | (, ) | Target initial position | (60 km, 20 km) | | Missile initial velocity | 1200 (m/s) | | Target initial velocity | 2000 (m/s) | | Missile initial flight path angle | 0 (deg) | | Target initial flight path angle | 0 (deg) | | Parameter of the controller | 10 or 30 | | Navigation ratio of PN | 3 |
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