Designing a robust nonlinear dynamic inversion controller for spacecraft formation flying

DOI10.1155/2014/471352zbMath1407.93273OpenAlexW2154095177WikidataQ59067536 ScholiaQ59067536MaRDI QIDQ1718463

Inseok Yang, Dongik Lee, Dong-Seog Han

Publication date: 8 February 2019

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2014/471352

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Automated systems (robots, etc.) in control theory (93C85) Control of mechanical systems (70Q05) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (3)

U-model-based double sliding mode control (U_DSM-control) of nonlinear dynamic systems ⋮ A unified approach to nonlinear dynamic inversion control with parameter determination by eigenvalue assignment ⋮ Time-delay robust nonlinear dynamic inversion for chaos synchronization with application to secure communications

Cites Work

• Differential geometric methods in variable-structure control
• Variable structure systems with sliding modes
• Dynamic inversion: an evolving methodology for flight control design

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