Virtual Target Based Terminal Guidance Law for Cruise Projectile Considering Impact Angle Constraint-Reference-Cited by-同舟云学术

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Virtual Target Based Terminal Guidance Law for Cruise Projectile Considering Impact Angle Constraint

Published:2023-07-24 Issue: Volume: Page:
ISSN:
Container-title:2023 42nd Chinese Control Conference (CCC)
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Author:

Li Guanlin¹,Yang Qiangwei¹,Huang Xudong¹

Affiliation:

1. AVIC XI'AN Flight automatic control research institute,Xi'an,710000

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10239690/10239711/10240335.pdf?arnumber=10240335

Reference11 articles.

1. Analysis of time-sensitive targets of air-to-surface guided munitions;zhu;Missile Aerodynamics,2014

2. Terminal Sliding Mode Control for Spacecraft Formation Flying

3. Finite time control guidance law for guided bombs considering impact angle constraints;mu;Navigation Positioning & Timing[J],2020

4. Adaptive integral sliding mode guidance law considering impact angel constraint;zhao;Control and Decision,2017

5. Design of optimal terminal guidance law for guided rockets;bian;Journal of Ballistics,2013

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Terminal Angle Constrained Three-Dimensional Disturbance Rejection Guidance via an Incremental Twisting Algorithm;2024 3rd Conference on Fully Actuated System Theory and Applications (FASTA);2024-05-10

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