Rigid Spacecraft Attitude Control Based on Finite‐Time Non‐Singular Sliding Mode and Extended State Disturbance Observer With Input Hysteresis.
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| Title: | Rigid Spacecraft Attitude Control Based on Finite‐Time Non‐Singular Sliding Mode and Extended State Disturbance Observer With Input Hysteresis. |
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| Authors: | Liu, Junjun1,2 (AUTHOR), Cui, Yufu2 (AUTHOR), Wang, Haoping1 (AUTHOR) hp.wang@njust.edu.cn, Tian, Yang1 (AUTHOR), Zhou, Xingyu3 (AUTHOR) |
| Source: | International Journal of Robust & Nonlinear Control. 7/10/2025, Vol. 35 Issue 10, p4187-4200. 14p. |
| Database: | Mathematics Source |
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| ISSN: | 10498923 |
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| DOI: | 10.1002/rnc.7896 |
