An adaptive Kalman filter design that utilizes recursive maximum likelihood parameter identification is discussed. At the center of this design is the Kalman filter itself, which has the responsibility for attitude determination. At the same time, the identification algorithm is continually identifying the system parameters. The approach is applicable to nonlinear, as well as linear systems. This adaptive Kalman filter design has much potential for real time implementation, especially considering the fast clock speeds, cache memory and internal RAM available today. The recursive maximum likelihood algorithm is discussed in detail, with special attention directed towards its unique matrix formulation. The procedure for using the algorithm is...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
In this paper, a comprehensive comparison of two robust estimation techniques namely, compensated cl...
In the interests of enhancing autonomous navigation capabilities for Low Earth Orbit formation flyin...
Attitude determination has been considered as a permanent topic of active research and perhaps remai...
Includes bibliographical references (page 82)In the early 1960???s Rudolf Emil Kalman published a re...
For spacecraft conducting on-orbit operations, changes to the structure of the spacecraft are not un...
In this paper, a Kalman filter formulation for attitude estimation is derived using the Modified Rod...
The Kalman filter is the general solution to the recursive, minimised mean square estimation problem...
This paper considers a novel method for estimating parameters in a vehicle handling dynamic model us...
Attitude estimation of earth orbiting satellites (including Large Space Telescope) subjected to envi...
Attitude determination is a major element of the operation and maintenance of a spacecraft. There ar...
An adaptive Kalman filtering approach is proposed for attitude determination to replace the fixed (...
Computer simulation results of attitude estimation of Earth-orbiting satellites (including Space Tel...
Prediction Algorithms for the Attitude Estimator The attitude estimator is an extended Kalman filte...
In part-1 of this paper an adaptive filtering based on a reference recursive recipe (RRR) was develo...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
In this paper, a comprehensive comparison of two robust estimation techniques namely, compensated cl...
In the interests of enhancing autonomous navigation capabilities for Low Earth Orbit formation flyin...
Attitude determination has been considered as a permanent topic of active research and perhaps remai...
Includes bibliographical references (page 82)In the early 1960???s Rudolf Emil Kalman published a re...
For spacecraft conducting on-orbit operations, changes to the structure of the spacecraft are not un...
In this paper, a Kalman filter formulation for attitude estimation is derived using the Modified Rod...
The Kalman filter is the general solution to the recursive, minimised mean square estimation problem...
This paper considers a novel method for estimating parameters in a vehicle handling dynamic model us...
Attitude estimation of earth orbiting satellites (including Large Space Telescope) subjected to envi...
Attitude determination is a major element of the operation and maintenance of a spacecraft. There ar...
An adaptive Kalman filtering approach is proposed for attitude determination to replace the fixed (...
Computer simulation results of attitude estimation of Earth-orbiting satellites (including Space Tel...
Prediction Algorithms for the Attitude Estimator The attitude estimator is an extended Kalman filte...
In part-1 of this paper an adaptive filtering based on a reference recursive recipe (RRR) was develo...
Satellite attitude determination by simulation program using Monte Carlo sampling and Kalman-Schmidt...
In this paper, a comprehensive comparison of two robust estimation techniques namely, compensated cl...
In the interests of enhancing autonomous navigation capabilities for Low Earth Orbit formation flyin...