In this paper, a sequential multiplicative extended Kalman filter (SMEKF) is proposed for attitude estimation using vector observations. In the proposed SMEKF, each of the vector observations is processed sequentially to update the attitude, which can make the measurement model linearization more accurate for the next vector observation. This is the main difference to Murrell’s variation of the MEKF, which does not update the attitude estimate during the sequential procedure. Meanwhile, the covariance is updated after all the vector observations have been processed, which is used to account for the special characteristics of the reset operation necessary for the attitude update. This is the main difference to the traditional sequentia...
Star trackers typically obtain attitude information about a vehicle by imaging a portion of the sky ...
The invariant unscented Kalman filtering (IUKF), relies on a geometrical-based constructive method f...
For a small satellite, the processor onboard the attitude determination and control system (ADCS) is...
This paper presents a novel attitude estimator called the multiplicative exogenous Kalman filter. Th...
Attitude estimation is often inaccurate during highly dynamic motion due to the external acceleratio...
This paper presents the implementation of an adaptive fading multiplicative extended Kalman filter (...
This work compares the performance of linear attitude estimators; in particular, the classic multipl...
In this paper, a new Kalman filtering scheme is designed in order to give the optimal attitude estim...
© 1963-2012 IEEE.This article proposes two novel covariance-tuning methods to form a robust Kalman f...
IEEE.This paper proposes a novel covariance-scaling based robust adaptive Kalman filter (RAKF) algor...
Abstract For invariant attitude dynamics evolving on matrix Lie groups, by proposing the stochastic ...
International audienceThis article proposes a new formulation to derive the invariant unscented Kalm...
International audienceThis paper proposes an attitude estimation methodology for the case where atti...
A sequential filtering algorithm is presented for attitude and attitude-rate estimation from Global ...
A current statistical model for maneuvering acceleration using an adaptive extended Kalman filter (C...
Star trackers typically obtain attitude information about a vehicle by imaging a portion of the sky ...
The invariant unscented Kalman filtering (IUKF), relies on a geometrical-based constructive method f...
For a small satellite, the processor onboard the attitude determination and control system (ADCS) is...
This paper presents a novel attitude estimator called the multiplicative exogenous Kalman filter. Th...
Attitude estimation is often inaccurate during highly dynamic motion due to the external acceleratio...
This paper presents the implementation of an adaptive fading multiplicative extended Kalman filter (...
This work compares the performance of linear attitude estimators; in particular, the classic multipl...
In this paper, a new Kalman filtering scheme is designed in order to give the optimal attitude estim...
© 1963-2012 IEEE.This article proposes two novel covariance-tuning methods to form a robust Kalman f...
IEEE.This paper proposes a novel covariance-scaling based robust adaptive Kalman filter (RAKF) algor...
Abstract For invariant attitude dynamics evolving on matrix Lie groups, by proposing the stochastic ...
International audienceThis article proposes a new formulation to derive the invariant unscented Kalm...
International audienceThis paper proposes an attitude estimation methodology for the case where atti...
A sequential filtering algorithm is presented for attitude and attitude-rate estimation from Global ...
A current statistical model for maneuvering acceleration using an adaptive extended Kalman filter (C...
Star trackers typically obtain attitude information about a vehicle by imaging a portion of the sky ...
The invariant unscented Kalman filtering (IUKF), relies on a geometrical-based constructive method f...
For a small satellite, the processor onboard the attitude determination and control system (ADCS) is...