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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.
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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RecordInfo BibRecord:
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        Value: 10.1049/cth2.70018
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      – Code: eng
        Text: English
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        PageCount: 15
        StartPage: 1
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      – TitleFull: 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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              Text: Jan2025
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              Y: 2025
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