Finite-Time Control for Satellite Formation Reconfiguration and Maintenance in LEO: A Nonlinear Lyapunov-Based SDDRE Approach

This paper introduces a nonlinear Lyapunov-based Finite-Time State-Dependent Differential Riccati Equation (FT-SDDRE) control scheme, considering actuator saturation constraints and ensuring that the control system operates within safe operational limits designed for satellite reconfiguration and fo...

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Bibliographic Details
Main Authors: Majid Bakhtiari, Amirhossein Panahyazdan, Ehsan Abbasali
Format: Article
Language:English
Published: MDPI AG 2025-02-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/12/3/201
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