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...

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Hlavní autoři:	Chao Lai, Weihong Wang, Zhenghua Liu, Tingting Liang, Shenao Yan
Médium:	Artigo
Jazyk:	Inglês
Vydáno:	IEEE 2018-01-01
Edice:	IEEE Access
Témata:	Adaptive control dynamic surface control extended state observer impact angle constraint partial integrated guidance and control terminal sliding mode control
On-line přístup:	https://ieeexplore.ieee.org/document/8468171/
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