We consider the problem of state and parameter estimation for geostationary spacecraft in an accurate and efficient way. For this purpose we implement a Jet Transport Taylor technique in two coordinate representations, analyzing the impact of using different orders in the computations. Then, under the assumption of a Gaussian distribution, we evaluate the mean vectors and covariance matrices corresponding to estimated states and parameters. These are incorporated into a high order Kalman filter where the estimates are updated sequentially. The performances on the orbit determination and parameter estimation are discussed by a series of numerical simulations which are compared with a classical implementation of the filter.Peer ReviewedPostpr...
this paper aims at identifying the best filtering approach to be used in relative orbit scenarios in...
ABSTRACT: In this paper a new Adaptive Unscented Kalman Filter (AUKF) is proposed and applied for th...
A novel method for efficient high-accuracy satellite attitude estimation is presented to address the...
We consider the problem of state and parameter estimation for geostationary spacecraft in an accurat...
Based on the jet transport technique, this paper proposes a novel nonlinear Kalman filter for simult...
111 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1986.This research compares the pe...
In self-assisted GNSS the orbit of a satellite is predicted by solving the differential equation tha...
In this paper, an orbit determination strategy that uses non-recursive batch filter, and unscented K...
Increasing satellite attitude requirements demand high accuracy estimation methods capable of operat...
This research assesses the performance of filtering schemes for tracking uncooperative satellites th...
The problem of nonlinear filtering represents a crucial issue in celestial mechanics. In this paper ...
The problem of nonlinear filtering represents a crucial issue in celestial mechanics. In this paper ...
The paper presents a new step-by-step procedure for constructing a navigation satellite motion model...
This paper presents the study of the orbit determination of near-circular, low-Earth orbit (LEO) spa...
International audienceSpaceborne gravity gradients are proposed in this paper to provide autonomous ...
this paper aims at identifying the best filtering approach to be used in relative orbit scenarios in...
ABSTRACT: In this paper a new Adaptive Unscented Kalman Filter (AUKF) is proposed and applied for th...
A novel method for efficient high-accuracy satellite attitude estimation is presented to address the...
We consider the problem of state and parameter estimation for geostationary spacecraft in an accurat...
Based on the jet transport technique, this paper proposes a novel nonlinear Kalman filter for simult...
111 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 1986.This research compares the pe...
In self-assisted GNSS the orbit of a satellite is predicted by solving the differential equation tha...
In this paper, an orbit determination strategy that uses non-recursive batch filter, and unscented K...
Increasing satellite attitude requirements demand high accuracy estimation methods capable of operat...
This research assesses the performance of filtering schemes for tracking uncooperative satellites th...
The problem of nonlinear filtering represents a crucial issue in celestial mechanics. In this paper ...
The problem of nonlinear filtering represents a crucial issue in celestial mechanics. In this paper ...
The paper presents a new step-by-step procedure for constructing a navigation satellite motion model...
This paper presents the study of the orbit determination of near-circular, low-Earth orbit (LEO) spa...
International audienceSpaceborne gravity gradients are proposed in this paper to provide autonomous ...
this paper aims at identifying the best filtering approach to be used in relative orbit scenarios in...
ABSTRACT: In this paper a new Adaptive Unscented Kalman Filter (AUKF) is proposed and applied for th...
A novel method for efficient high-accuracy satellite attitude estimation is presented to address the...