Barrier Lyapunov function-based integrated guidance and control with input saturation and state constraints-Reference-Cited by-同舟云学术

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Barrier Lyapunov function-based integrated guidance and control with input saturation and state constraints

Published:2019-01 Issue: Volume:84 Page:845-855
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Liu Wangkui,Wei Yiyin,Duan Guangren

Funder

Major Program of National Natural Science Foundation of China

National Natural Science Foundation of China

Self-Planned Task of State Key Laboratory of Robotics and System (HIT)

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference38 articles.

1. Integrated guidance and control of missiles with θ–D method;Xin;IEEE Trans. Control Syst. Technol.,2004

2. Integrated guidance and control design of the suicide UCAV for terminal attack;Zhou;J. Syst. Eng. Electron.,2017

3. Continuous-time predictive control-based integrated guidance and control;Panchal;J. Guid. Control Dyn.,2017

4. Finite horizon integrated guidance and control for terminal homing in vertical plane;Kim;J. Guid. Control Dyn.,2016

5. A new sliding mode control design for integrated missile guidance and control system;Guo;Aerosp. Sci. Technol.,2018

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