An Adaptive Sliding Mode Terminal Guidance Method-Reference-Cited by-同舟云学术

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An Adaptive Sliding Mode Terminal Guidance Method

Published:2023-11-17 Issue: Volume:35 Page:7834-7839
ISSN:
Container-title:2023 China Automation Congress (CAC)
language:
Short-container-title:

Author:

Zhu Yichuan¹,Yao Na²,Fan Hu³

Affiliation:

1. Beijing Aerospace Automatic Control Institute,National Key Laboratory of Science and Technology on Aerospace Intelligence Control,Beijing,China

2. Beijing Aerospace Automatic Control Institute,System simulation laboratory,Beijing,China

3. The third representative office of air force equipment in Beijing area,Beijing,China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10450150/10449968/10450493.pdf?arnumber=10450493

Reference10 articles.

1. Impact Time and Angle Control Based on Constrained Optimal Solutions

2. Modified Pure Proportional Navigation Guidance Law for Impact Time Control

3. Two-phase guidance law for impact time control under physical constraints

4. Optimal Intermediate Guidance Law with Angle Constraints Considering the Time Varying Speed of Missiles;Xiong;Control theory and application,2018

5. Parameter Adjustable Optimal Guidance Law with Falling Angle Constraint [J];Zhang;Flight mechanics,2021

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