Terminal Sliding Mode Control for Spacecraft Formation Flying

Author:

Hui Liu,Li Junfeng

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Cited by 114 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. Fully Distributed Formation Flying Control of Multiple Spacecraft by Observer-Based Linear Output Protocols;IEEE Transactions on Aerospace and Electronic Systems;2023-12

2. Robust non-aggressive three-axis attitude control of spacecraft: dynamic sliding mode approach;Control Theory and Technology;2023-11

3. Time-varying distributed optimization problem with inequality constraints;Journal of the Franklin Institute;2023-11

4. Fault-tolerant cooperative control for a class of satellite formation;2023 CAA Symposium on Fault Detection, Supervision and Safety for Technical Processes (SAFEPROCESS);2023-09-22

5. Virtual Target Based Terminal Guidance Law for Cruise Projectile Considering Impact Angle Constraint;2023 42nd Chinese Control Conference (CCC);2023-07-24

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