Abstract — This paper presents the design, analysis, and performance evaluation of globally asymptotically stable filters for attitude estimation. The design is based directly on the sensor measurements as opposed to traditional solutions that resort to parameterizations of the rotation, e.g., Euler angles or quaternions, or more recent geometric approaches explicitly solved on the special orthogonal group, SO(3). The proposed solutions include the estimation of gyro bias, incomplete sensor measurements, systematic tuning procedures, and also allow for the inclusion of frequency weights to model colored noise. Finally, and due to the inherent structure, the filters are comple-mentary and also cope well with slowly time-varying gyro bias. Si...
We consider the attitude and gyro-bias estimation as well as the attitude stabilization problem of a...
In this paper, a new Kalman filtering scheme is designed in order to give the optimal attitude estim...
This paper considers the question of using a nonlinear complementary filter for attitude estimation ...
16International audienceThis paper considers the problem of obtaining good attitude estimates from m...
International audienceFocusing on generalized sensor combinations, this paper deals with attitude es...
International audienceThis paper proposes a novel quaternion-basedattitude estimator with magnetic, ...
International audienceThis brief proposes new algorithms for attitude estimation and control, based ...
This chapter presents a complete development of a complementary filter-based attitude estimation sch...
This paper considers the question of obtaining high quality attitude estimates from typical low cost...
Aircraft attitude estimation requires fusing several sensors in order to recover both high and low f...
The attitude control problem, or the control of a spacecraft's orientation with respect to a frame o...
Copyright: © 2021 by the authors. Attitude estimation is the process of computing the orientation an...
This paper presents a novel attitude estimator called the multiplicative exogenous Kalman filter. Th...
© 2019 IEEE.All attitude filter designers are familiar with the covariance matrix tuning process for...
Abstract — This paper concerns the problem of position and attitude estimation based on the fusion o...
We consider the attitude and gyro-bias estimation as well as the attitude stabilization problem of a...
In this paper, a new Kalman filtering scheme is designed in order to give the optimal attitude estim...
This paper considers the question of using a nonlinear complementary filter for attitude estimation ...
16International audienceThis paper considers the problem of obtaining good attitude estimates from m...
International audienceFocusing on generalized sensor combinations, this paper deals with attitude es...
International audienceThis paper proposes a novel quaternion-basedattitude estimator with magnetic, ...
International audienceThis brief proposes new algorithms for attitude estimation and control, based ...
This chapter presents a complete development of a complementary filter-based attitude estimation sch...
This paper considers the question of obtaining high quality attitude estimates from typical low cost...
Aircraft attitude estimation requires fusing several sensors in order to recover both high and low f...
The attitude control problem, or the control of a spacecraft's orientation with respect to a frame o...
Copyright: © 2021 by the authors. Attitude estimation is the process of computing the orientation an...
This paper presents a novel attitude estimator called the multiplicative exogenous Kalman filter. Th...
© 2019 IEEE.All attitude filter designers are familiar with the covariance matrix tuning process for...
Abstract — This paper concerns the problem of position and attitude estimation based on the fusion o...
We consider the attitude and gyro-bias estimation as well as the attitude stabilization problem of a...
In this paper, a new Kalman filtering scheme is designed in order to give the optimal attitude estim...
This paper considers the question of using a nonlinear complementary filter for attitude estimation ...