Terminal Sliding Mode Control for Spacecraft Formation Flying

By Liu Hui, Junfeng Li. IEEE Transactions on Aerospace and Electronic Systems, 2009

179 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Astronomy and Astrophysics, Computer Networks and Communications

View Paper: https://www.semanticscholar.org/paper/12e05321deb47e9c639b08183490cdde7d79b664

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Zhihong Man
2. Zhao-wei Sun
3. Jianying Wang
4. Yong Feng
5. Jinzhi Wang
6. Xianghua Wang
7. Xinghuo Yu

In Astronomy and Astrophysics

1. Zhihong Man
2. Zhao-wei Sun
3. Jianying Wang
4. Yong Feng
5. Xinghuo Yu

In Computer Networks and Communications

1. Xinghuo Yu
2. Yong Feng
3. Zhihong Man
4. Zhao-wei Sun
5. Jianying Wang
6. Ming Liu

Citations in the corpus

• Terminal Sliding Mode Control – An Overview (2021, methodology): “In [116], a TSMC was designed for spacecraft formation.”
• Partial Integrated Missile Guidance and Control with Finite Time Convergence (2013, background): “The conventional linear sliding mode control [2,3], whose sliding surface is a linear function of the tracking error and its derivatives, can only achieve the asymptotic convergence in the sliding phase, whereas the finite time convergence may be accomplished by the terminal sliding mode control (TS”
• Finite-Time Control for Spacecraft Formation with Dual-Number-Based Description (2012, methodology): “On the other hand, the terminal sliding mode (TSM) control has been applied successfully in the spacecraft attitude tracking control [21] and SFF orbit reconfiguration control [22].”