Three-Dimensional Impact Angle Constrained Partial Integrated Guidance and Control With Finite-Time Convergence

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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Bibliographic Details
Main Authors: Chao Lai, Weihong Wang, Zhenghua Liu, Tingting Liang, Shenao Yan
Format: Article
Language:English
Published: IEEE 2018-01-01
Series:IEEE Access
Subjects:
Adaptive control
dynamic surface control
extended state observer
impact angle constraint
partial integrated guidance and control
terminal sliding mode control
Online Access:https://ieeexplore.ieee.org/document/8468171/

Internet

https://ieeexplore.ieee.org/document/8468171/

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