Missile Guidance Laws Based on SMC and FTC Techniques
Missile Guidance Laws Based on SMC and FTC Techniques
- New search for: Xia, Yuanqing
- New search for: Fu, Mengyin
- New search for: Xia, Yuanqing
- New search for: Fu, Mengyin
Proportional navigation (PN) has attracted a amount of interest in the missile interception and design of guidance laws due to the high effectiveness and simple implementation [299, 332, 221, 7]. Specially, PN guidance laws can be easily applied to many-to-one engagement scenarios and achieve the cooperative simultaneous attack of multiple missiles against their common target [123]. However, the PN guidance law is more applicable for the task of intercepting a non-maneuvering target or a weakly maneuvering target. In practice, target acceleration can change rapidly. For intercepting a target with powerful maneuvering capability, the performance of PN is degraded and it may be ineffective for some orientations between missile and target.
Document information
Missile Guidance Laws Based on SMC and FTC Techniques
Lect.Notes Control
2013-01-01
14 pages
Article/Chapter (Book)
Electronic Resource
English
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