Spin Recovery of High‐Angle‐of‐Attack Aircraft With Altitude Gain Reduction in the Presence of Aerodynamic Uncertainty: A MIMO Super‐Twisting Sliding Mode Approach.
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| Title: | Spin Recovery of High‐Angle‐of‐Attack Aircraft With Altitude Gain Reduction in the Presence of Aerodynamic Uncertainty: A MIMO Super‐Twisting Sliding Mode Approach. |
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| Authors: | Bagheri, Ahmad1 (AUTHOR), Danesh, Mohammad1 (AUTHOR) danesh@iut.ac.ir |
| Source: | IET Control Theory & Applications (Wiley-Blackwell). Jan2025, Vol. 19 Issue 1, p1-15. 15p. |
| Database: | Mathematics Source |
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| ISSN: | 17518644 |
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| DOI: | 10.1049/cth2.70018 |
