Configuration flatness of Lagrangian systems underactuated by one control

Lagrangian control systems that are differentially flat with flat outputs that only depend on configuration variables are said to be configuration flat. We provide a complete characterisation of configuration flatness for systems with n degrees of freedom and n-1 controls whose range of control forces only depends on configuration and whose Lagrangian has the form of kinetic energy minus potential. The method presented allows us to determine if such a system is configuration flat and, if so provides a constructive method for finding all possible configuration flat outputs. Our characterisation relates configuration flatness to Riemannian geometry.

[1]  H. J.,et al.  Hydrodynamics , 1924, Nature.

[2]  Ralph Abraham,et al.  Foundations Of Mechanics , 2019 .

[3]  J. Lévine,et al.  On dynamic feedback linearization , 1989 .

[4]  D. Saunders The Geometry of Jet Bundles , 1989 .

[5]  W. Shadwick,et al.  Absolute equivalence and dynamic feedback linearization , 1990 .

[6]  Philippe Martin Contribution a l'etude des systemes differentiellement plats , 1992 .

[7]  M. Fliess,et al.  Linéarisation par bouclage dynamique et transformations de Lie-Bäcklund , 1993 .

[8]  M. Fliess,et al.  Flatness, motion planning and trailer systems , 1993, Proceedings of 32nd IEEE Conference on Decision and Control.

[9]  R. Murray,et al.  Differential flatness and absolute equivalence , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.

[10]  B. Paden,et al.  A different look at output tracking: control of a VTOL aircraft , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.

[11]  M. Fliess,et al.  Flatness and defect of non-linear systems: introductory theory and examples , 1995 .

[12]  Jean-Baptiste Pomet A differential geometric setting for dynamic equivalence and dynamic linearization , 1995 .

[13]  M.J. van Nieuwstadt,et al.  Approximate trajectory generation for differentially flat systems with zero dynamics , 1995, Proceedings of 1995 34th IEEE Conference on Decision and Control.

[14]  R. Murray,et al.  Differential Flatness of Mechanical Control Systems: A Catalog of Prototype Systems , 1995 .

[15]  R. Murray,et al.  Trajectory generation for the N-trailer problem using Goursat normal form , 1995 .

[16]  A different look at output tracking: control of a vtol aircraft , 1996, Autom..

[17]  Muruhan Rathinam,et al.  A Test for Differential Flatness by Reduction to Single Input Systems , 1996 .

[18]  D. M. Tilbury,et al.  A bound on the number of integrators needed to linearize a control system , 1996 .

[19]  A. D. Lewis,et al.  Configuration Controllability of Simple Mechanical Control Systems , 1997 .

[20]  R. Murray,et al.  Configuration Flatness of Lagrangian Systems Underactuated by One Control , 1998 .