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Output feedback continuous terminal sliding mode guidance law for missile-target interception with autopilot dynamics

Zhao, Zhenhua, Li, Chuntao, Yang, Jun, Li, Shihua
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Language:
english
Journal:
Aerospace Science and Technology
DOI:
10.1016/j.ast.2019.01.012
Date:
January, 2019
File:
PDF, 1.77 MB
english, 2019
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