In this contribution the optimal stabilization problem of periodic orbits is studied in a symplectic geometry setting. For this, the stable manifold theory for the point stabilization case is generalized to the case of periodic orbit stabilization. Sufficient conditions for the existence of a \gls{nhim} of the Hamiltonian system are derived. It is shown that the optimal control problem has a solution if the related periodic Riccati equation has a unique periodic solution. For the analysis of the stable and unstable manifold a coordinate transformation is used which is moving along the orbit. As an example, an optimal control problem is considered for a spring mass oscillator system, which should be stabilized at a certain energy level.Comme...
In this paper we propose an improved method for calculating Henon's stability parameter, which is ba...
Stability of periodic and equilibrium solutions of restricted three-body problems - measure preservi...
In the circular restricted three-body problem, low energy transit orbits are revealed by linearizing...
In this contribution the optimal stabilization problem of periodic orbits is studied in a symplectic...
Le problème principalement étudié dans ce manuscrit est la stabilisation d orbites périodiques de sy...
International audienceThis paper tackles in the stabilization of periodic orbits of nonlinear discre...
Efficient and robust numerical methods for solving the periodic Riccati differential equation (PRDE)...
Abstract: This paper provides an introduction to several problems and techniques related to controll...
A systematic research on the structure-preserving controller is investigated in this paper, includin...
In this Letter we consider the stabilization problem of unstable periodic orbits of discrete time ch...
AbstractIn this paper, we derive a result for stabilizability and a separation principle for periodi...
Orbital stabilization is a particular form of set stabilization, where the control objective is to i...
Instability of periodic orbits in restricted and reduced three-body problems using mapping by fixed ...
Efficient and robust numerical methods for solving the periodic Riccati differential equation (PRDE)...
Part 4: Stabilization, Feedback, and Model Predictive ControlInternational audienceIn optimal contro...
In this paper we propose an improved method for calculating Henon's stability parameter, which is ba...
Stability of periodic and equilibrium solutions of restricted three-body problems - measure preservi...
In the circular restricted three-body problem, low energy transit orbits are revealed by linearizing...
In this contribution the optimal stabilization problem of periodic orbits is studied in a symplectic...
Le problème principalement étudié dans ce manuscrit est la stabilisation d orbites périodiques de sy...
International audienceThis paper tackles in the stabilization of periodic orbits of nonlinear discre...
Efficient and robust numerical methods for solving the periodic Riccati differential equation (PRDE)...
Abstract: This paper provides an introduction to several problems and techniques related to controll...
A systematic research on the structure-preserving controller is investigated in this paper, includin...
In this Letter we consider the stabilization problem of unstable periodic orbits of discrete time ch...
AbstractIn this paper, we derive a result for stabilizability and a separation principle for periodi...
Orbital stabilization is a particular form of set stabilization, where the control objective is to i...
Instability of periodic orbits in restricted and reduced three-body problems using mapping by fixed ...
Efficient and robust numerical methods for solving the periodic Riccati differential equation (PRDE)...
Part 4: Stabilization, Feedback, and Model Predictive ControlInternational audienceIn optimal contro...
In this paper we propose an improved method for calculating Henon's stability parameter, which is ba...
Stability of periodic and equilibrium solutions of restricted three-body problems - measure preservi...
In the circular restricted three-body problem, low energy transit orbits are revealed by linearizing...