Robust terminal guidance law design for missiles against maneuvering targets-Reference-Cited by-同舟云学术

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Robust terminal guidance law design for missiles against maneuvering targets

Published:2016-07 Issue: Volume:54 Page:198-207
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Chen Yung-Yue^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference20 articles.

1. Guidance;Locke,1995

2. Modern Navigation, Guidance, and Control Processing;Ching-Fang,1991

3. Design of a CLOS guidance law via feedback linearization;In-Joong;IEEE Trans. Aerosp. Electron. Syst.,1992

4. Tactical and Strategic Missile Guidance;Paul,1990

5. General guidance law for homing missile;Ciann-Dong;IEEE Trans. Aerosp. Electron. Syst.,1989

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2. An active disturbance rejection control guidance law based collision avoidance for unmanned aerial vehicles;Aerospace Science and Technology;2018-06

3. Robust finite-time guidance against maneuverable targets with unpredictable evasive strategies;Aerospace Science and Technology;2018-06

4. A constant guidance law-based collision avoidance for unmanned aerial vehicles;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2018-01-09

5. Two-Dimensional Continuous Terminal Interception Guidance Law With Predefined Convergence Performance;IEEE Access;2018

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