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Updated: Sep 24, 2025

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Published on: May 25, 2019
A Linear Time-Varying Inequality Approach for Prescribed Time Stability and Stabilization
This study unifies finite-time, fixed-time, and prescribed-time stability analysis using a linear time-varying inequality approach. This method enables effective prescribed-time stabilization for spacecraft attitude control systems.
Area of Science:
- Control Systems Engineering
- Nonlinear Dynamics
- Aerospace Engineering
Background:
- Traditional stability analysis methods often focus on asymptotic or exponential convergence.
- Finite-time and fixed-time stability offer faster convergence but lack unified frameworks.
- Prescribed-time stability allows for explicit control over convergence time, crucial for real-time applications.
Purpose of the Study:
- To develop a unified framework for analyzing finite-time, fixed-time, and prescribed-time stability.
- To introduce a novel linear time-varying (LTV) inequality-based approach for stability analysis.
- To solve the global prescribed-time stabilization problem for a rigid spacecraft attitude control system.
Main Methods:
- Introduction of a linear time-varying (LTV) inequality-based approach for prescribed-time stability analysis.
- Recasting existing nonlinear Lyapunov inequalities for finite- and fixed-time stability into the unified LTV framework.
- Application of the unified LTV approach to design a bounded nonlinear time-varying controller for spacecraft attitude stabilization using backstepping.
Main Results:
- Demonstration of the unified LTV inequality-based approach for analyzing various time-domain stabilities.
- Successful application of the unified framework to address the global prescribed-time stabilization of a rigid spacecraft.
- Development and validation of a bounded nonlinear time-varying controller for disturbance rejection.
Conclusions:
- The proposed LTV inequality-based approach provides a unified and effective method for finite-time, fixed-time, and prescribed-time stability analysis and stabilization.
- The developed controller ensures global prescribed-time stabilization for the spacecraft attitude control system, even under disturbance.
- Numerical simulations confirm the efficacy of the unified approach and the proposed control strategy.
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