Configuration flatness of Lagrangian control systems with fewer controls than degrees of freedom
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Publication:414572
DOI10.1016/j.sysconle.2011.11.007zbMath1238.93030OpenAlexW2077140783MaRDI QIDQ414572
Publication date: 11 May 2012
Published in: Systems \& Control Letters (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.sysconle.2011.11.007
Cites Work
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- On necessary and sufficient conditions for differential flatness
- Accurate modeling and robust hovering control for a quad-rotor VTOL aircraft
- Direct method based control system for an autonomous quadrotor
- Analysis and control of nonlinear systems. A flatness-based approach
- Flat output characterization for linear systems using polynomial matrices.
- Feedback linearization and driftless systems
- A different look at output tracking: Control of a VTOL aircraft
- Regression and the Moore-Penrose pseudoinverse
- Real-time trajectory generation for differentially flat systems
- Configuration Controllability of Simple Mechanical Control Systems
- On dynamic feedback linearization of four-dimensional affine control systems with two inputs
- Configuration Flatness of Lagrangian Systems Underactuated by One Control
- A Lie-Backlund approach to equivalence and flatness of nonlinear systems
- Flatness and defect of non-linear systems: introductory theory and examples
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