Motivated by real-world applications with intermittent sensor data, an extended Kalman filter is formulated as a hybrid system and constructive conditions on its parameters guaranteeing an asymptotic stability property are provided. The dynamical properties of the estimation error are first characterized infinitesimally so to yield bounds on the rate of convergence and overshoot that depend on the parameters. By recasting the problem as the stabilization of a compact set, robustness properties of the proposed algorithm in the presence of disturbances in the system dynamics as well as measurement noise in the output are established. The proposed strategy is applied to spacecraft relative motion control with position-only measurements
Kalman filter estimates the state of a dynamic system, even if the precise form of the system is unk...
Abstract: Construction of algorithm of extended Kalman filter for a nonlinear continuous -...
A filter is consistent if predicted errors are at least as large as actual errors. In this paper, we...
This thesis provides a novel approach to the problem of state estimation for discrete-time nonlinea...
Abstract—The Kalman filter and its extensions has been widely studied and applied in positioning, in...
Abstract—In this correspondence paper, a novel robust extended Kalman filter (REKF) for discrete-tim...
In normal working conditions it is possible to achieve sufficient attitude estimation accuracy for a...
This paper mainly focuses on the maneuver of the satellite in orbit. A non-linear multi-inputs multi...
In the interests of enhancing autonomous navigation capabilities for Low Earth Orbit formation flyin...
grantor: University of TorontoSpacecraft requirements are changing. Smaller, lower-cost sp...
To be published in IFAC world congress 2017 proceedingsIn the aerospace industry the (multiplicative...
In this paper, we propose a robust adaptive cubature Kalman filter (CKF) to deal with the problem of...
Recent developments in the field of automation and control have motivated the use of new approaches ...
We present some optimality results for robust Kalman filtering. To this end, we introduce the genera...
Estimation problems have to be solved in several space applications. During rendezvous to a target s...
Kalman filter estimates the state of a dynamic system, even if the precise form of the system is unk...
Abstract: Construction of algorithm of extended Kalman filter for a nonlinear continuous -...
A filter is consistent if predicted errors are at least as large as actual errors. In this paper, we...
This thesis provides a novel approach to the problem of state estimation for discrete-time nonlinea...
Abstract—The Kalman filter and its extensions has been widely studied and applied in positioning, in...
Abstract—In this correspondence paper, a novel robust extended Kalman filter (REKF) for discrete-tim...
In normal working conditions it is possible to achieve sufficient attitude estimation accuracy for a...
This paper mainly focuses on the maneuver of the satellite in orbit. A non-linear multi-inputs multi...
In the interests of enhancing autonomous navigation capabilities for Low Earth Orbit formation flyin...
grantor: University of TorontoSpacecraft requirements are changing. Smaller, lower-cost sp...
To be published in IFAC world congress 2017 proceedingsIn the aerospace industry the (multiplicative...
In this paper, we propose a robust adaptive cubature Kalman filter (CKF) to deal with the problem of...
Recent developments in the field of automation and control have motivated the use of new approaches ...
We present some optimality results for robust Kalman filtering. To this end, we introduce the genera...
Estimation problems have to be solved in several space applications. During rendezvous to a target s...
Kalman filter estimates the state of a dynamic system, even if the precise form of the system is unk...
Abstract: Construction of algorithm of extended Kalman filter for a nonlinear continuous -...
A filter is consistent if predicted errors are at least as large as actual errors. In this paper, we...