Design of Terminal Sliding Mode Attack Guidance Law with Impact Angle Constraint-Reference-Cited by-同舟云学术

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Design of Terminal Sliding Mode Attack Guidance Law with Impact Angle Constraint

Published:2024-06-07 Issue: Volume: Page:1122-1127
ISSN:
Container-title:2024 39th Youth Academic Annual Conference of Chinese Association of Automation (YAC)
language:
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Author:

Han Shuo¹,Mo Bo¹,Liu Chen²,Li Wenli³,Xu Junwei¹,Ren Fuhan⁴

Affiliation:

1. Beijing Institute of Technology,School of Aerospace Engineering,Beijing,China

2. CLP Intelligent (Beijing) Technology Co., Ltd.,Beijing,China

3. Wuhan Textile University,School of Management,Wuhan,China

4. Shandong Institute of Aerospace Electronics Technology,Yantai,China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10598401/10598402/10598624.pdf?arnumber=10598624

Reference18 articles.

1. Bias-Shaping Method for Biased Proportional Navigation with Terminal-Angle Constraint

2. Stochastic optimal control guidance law with bounded acceleration

3. Nonsingular Terminal Sliding Mode Guidance with Impact Angle Constraints

4. Adaptive Sliding Mode Relative Motion Control for Autonomous Carrier Landing of Fixed-Wing Unmanned Aerial Vehicles

5. Line-of-sight rate estimation and linearizing control of an imaging seeker in a tactical missile guided by proportional navigation

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