Fixed-Time Aircraft Spin Recovery Control Based on a Nonsingular Integral Terminal Sliding Mode Approach

Fixed-Time Aircraft Spin Recovery Control Based on a Nonsingular Integral Terminal Sliding Mode Approach

This paper introduces a control strategy to recover from various spin motions to level trim flight conditions, utilizing a fixed-time nonsingular terminal sliding mode approach to minimize altitude loss. Firstly, an integral terminal sliding mode surface is constructed to guarantee the tracking erro...

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Bibliographic Details
Main Authors: Huaji Wang, Xunnian Wang, Zhenglong Zhu, Lai Yan, Yu Yang
Format: Article
Language:English
Published: MDPI AG 2024-02-01
Series:Applied Sciences
Subjects:
spin recovery
terminal sliding mode
fixed time control
altitude loss minimization
Online Access:https://www.mdpi.com/2076-3417/14/5/1953

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