Three-Dimensional Impact Angle Constrained Partial Integrated Guidance and Control With Finite-Time Convergence
A 3-D impact angle constrained partial integrated guidance and control design with finite-time convergence is developed for a surface-to-air skid-to-turn missile intercepting a head-on maneuvering target. First, fully considering coupling among three channels and roll dynamics of missile, a new 3-D...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
IEEE
2018-01-01
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| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/8468171/ |