International audienceFocusing on generalized sensor combinations, this paper deals with attitude estimation problem using a linear complementary filter. The quaternion observation model is obtained via a gradient descent algorithm (GDA). An additive measurement model is then established according to derived results. The filter is named as the generalized complementary filter (GCF) where the observation model is simplified to its limit as a linear one that is quite different from previous-reported brute-force computation results. Moreover, we prove that representative derivative-based optimization algorithms are essentially equivalent to each other. Derivations are given to establish the state model based on the quaternion kinematic equatio...
This paper presents the Quaternion-based Robust Adaptive Unscented Kalman Filter (QRAUKF) for attitu...
[[abstract]]Obtaining precise attitude information is essential for aircraft navigation and control....
The attitude control problem, or the control of a spacecraft's orientation with respect to a frame o...
International audienceFocusing on generalized sensor combinations, this paper deals with attitude es...
This paper extents the by now classic sensor fusion complementary filter (CF) design, involving two ...
Aircraft attitude estimation requires fusing several sensors in order to recover both high and low f...
We present an application of a complementary filter system to the attitude determination of a remote...
International audienceAttitude estimation from vector observations is widely employed in aerospace a...
International audienceThis paper proposes a novel quaternion-basedattitude estimator with magnetic, ...
International audienceAs a key problem for multi-sensor attitudedetermination, Wahba’s problem has b...
Abstract — This paper presents the design, analysis, and performance evaluation of globally asymptot...
This contribution deals with attitude estimation algorithm based on measuring angular rate, earth ma...
Obtaining precise attitude information is essential for aircraft navigation and control. This paper ...
[[abstract]]Obtaining precise attitude information is essential for aircraft navigation and control....
In robot inertial navigation systems, to deal with the problems of drift and noise in the gyroscope ...
This paper presents the Quaternion-based Robust Adaptive Unscented Kalman Filter (QRAUKF) for attitu...
[[abstract]]Obtaining precise attitude information is essential for aircraft navigation and control....
The attitude control problem, or the control of a spacecraft's orientation with respect to a frame o...
International audienceFocusing on generalized sensor combinations, this paper deals with attitude es...
This paper extents the by now classic sensor fusion complementary filter (CF) design, involving two ...
Aircraft attitude estimation requires fusing several sensors in order to recover both high and low f...
We present an application of a complementary filter system to the attitude determination of a remote...
International audienceAttitude estimation from vector observations is widely employed in aerospace a...
International audienceThis paper proposes a novel quaternion-basedattitude estimator with magnetic, ...
International audienceAs a key problem for multi-sensor attitudedetermination, Wahba’s problem has b...
Abstract — This paper presents the design, analysis, and performance evaluation of globally asymptot...
This contribution deals with attitude estimation algorithm based on measuring angular rate, earth ma...
Obtaining precise attitude information is essential for aircraft navigation and control. This paper ...
[[abstract]]Obtaining precise attitude information is essential for aircraft navigation and control....
In robot inertial navigation systems, to deal with the problems of drift and noise in the gyroscope ...
This paper presents the Quaternion-based Robust Adaptive Unscented Kalman Filter (QRAUKF) for attitu...
[[abstract]]Obtaining precise attitude information is essential for aircraft navigation and control....
The attitude control problem, or the control of a spacecraft's orientation with respect to a frame o...