International audienceIn this paper we propose a nonlinear observer (i.e. a “filter”) to estimate the position and velocity vectors and the orientation of a flying rigid body, using measurements from low-cost Earth-fixed position and velocity, inertial and magnetic sensors. It has by design a nice geometrical structure appealing from an engineering viewpoint; it is easy to tune, computationally very economic, and with guaranteed (at least local) convergence around every “smooth” trajectory. Moreover, it sensibly behaves in the presence of magnetic disturbances. We illustrate its good performance on experimental comparisons with a commercial system, and demonstrate its simplicity by implementing it on an 8-bit microcontroller
International audienceThis paper studies heading estimation jointly with the attitude and position e...
This paper describes the design, analysis, and experimental results of an Attitude and Heading Syste...
Abstract-This paper develops a physical model of an inertial/magnetic measurement unit by effectivel...
International audienceA nonlinear observer (i.e. a “filter”) is proposed for estimating the attitude...
International audienceIn this paper we propose an invariant nonlinear observer (i.e. a “filter”) for...
International audienceIn this paper we propose invariant nonlinear observers for attitude and headin...
International audienceWe generalize several recent works on nonlinear observers for aided attitude h...
This paper deals with the attitude estimation of a rigid body equipped with angular velocity sensors...
This paper describes the design, analysis, and experimental results of an Attitude and Heading Syste...
This paper describes the design, analysis, and experimental results of an Attitude and Heading Syste...
Abstract-A cheap tourism airplane ADAHRS unit is developed by fusing magnetometers, rate gyros and a...
A low-cost attitude system has been developed for an ultrahigh altitude flight experiment. The exper...
The paper presents an innovative strategy to measure the initial heading of a vehicle in the local r...
A development procedure for a low-cost attitude and heading reference system (AHRS) with a self-deve...
This paper proposes a low cost and small size attitude and heading reference system based on MEMS in...
International audienceThis paper studies heading estimation jointly with the attitude and position e...
This paper describes the design, analysis, and experimental results of an Attitude and Heading Syste...
Abstract-This paper develops a physical model of an inertial/magnetic measurement unit by effectivel...
International audienceA nonlinear observer (i.e. a “filter”) is proposed for estimating the attitude...
International audienceIn this paper we propose an invariant nonlinear observer (i.e. a “filter”) for...
International audienceIn this paper we propose invariant nonlinear observers for attitude and headin...
International audienceWe generalize several recent works on nonlinear observers for aided attitude h...
This paper deals with the attitude estimation of a rigid body equipped with angular velocity sensors...
This paper describes the design, analysis, and experimental results of an Attitude and Heading Syste...
This paper describes the design, analysis, and experimental results of an Attitude and Heading Syste...
Abstract-A cheap tourism airplane ADAHRS unit is developed by fusing magnetometers, rate gyros and a...
A low-cost attitude system has been developed for an ultrahigh altitude flight experiment. The exper...
The paper presents an innovative strategy to measure the initial heading of a vehicle in the local r...
A development procedure for a low-cost attitude and heading reference system (AHRS) with a self-deve...
This paper proposes a low cost and small size attitude and heading reference system based on MEMS in...
International audienceThis paper studies heading estimation jointly with the attitude and position e...
This paper describes the design, analysis, and experimental results of an Attitude and Heading Syste...
Abstract-This paper develops a physical model of an inertial/magnetic measurement unit by effectivel...