The paper deals with model-based attitude estimation for multicopters and is mainly focused on investigation of accuracy degradation due to wind and inaccurate model parameters which are conditions always present when using in real world. At first the need for model-base estimation is motivated. Then the multicopter model is described. Based on the mathematical model of multicopter, the estimation algorithm utilizing the extended Kalman filter is constructed. The main contribution of the paper is the investigation of the negative impact of the wind and of inaccurate knowledge of the model parameters
This chapter presents a complete development of a complementary filter-based attitude estimation sch...
International audienceA robust and reliable attitude estimator is a key technology enabler for the d...
AbstractUnmanned helicopters have been used extensively in the last few decades as a research platfo...
This dissertation deals with attitude estimation of multicopters. Mainly the use of multicopter dyna...
The paper is focused on attitude estimation of multicopters. Specifically the use of dynamic model o...
This thesis deals with attitude measurement by fusing sensor information from accelerometers, gyros ...
This paper presents an extended Kalman filter (EKF) for estimating the attitude and heading for guid...
This contribution deals with attitude estimation algorithm based on measuring angular rate, earth ma...
This paper discusses the evaluation of a novel attitude estimation algorithm (Kamali et al.(2013)) f...
Sensor measurements are corrupted by biases, noise and drift effects and, in order to provide accura...
International audienceThis paper deals with the attitude estimation of a quadrotor in the presence o...
This article deals with the problem of attitude control of multicopters. At first the basic properti...
Attitude estimation is often inaccurate during highly dynamic motion due to the external acceleratio...
This paper analyzes the performance of an Extended Kalman Filter (EKF) based attitude estimator for...
This paper puts forward Kalman filter algorithm to improve the accuracy and the stability of four ro...
This chapter presents a complete development of a complementary filter-based attitude estimation sch...
International audienceA robust and reliable attitude estimator is a key technology enabler for the d...
AbstractUnmanned helicopters have been used extensively in the last few decades as a research platfo...
This dissertation deals with attitude estimation of multicopters. Mainly the use of multicopter dyna...
The paper is focused on attitude estimation of multicopters. Specifically the use of dynamic model o...
This thesis deals with attitude measurement by fusing sensor information from accelerometers, gyros ...
This paper presents an extended Kalman filter (EKF) for estimating the attitude and heading for guid...
This contribution deals with attitude estimation algorithm based on measuring angular rate, earth ma...
This paper discusses the evaluation of a novel attitude estimation algorithm (Kamali et al.(2013)) f...
Sensor measurements are corrupted by biases, noise and drift effects and, in order to provide accura...
International audienceThis paper deals with the attitude estimation of a quadrotor in the presence o...
This article deals with the problem of attitude control of multicopters. At first the basic properti...
Attitude estimation is often inaccurate during highly dynamic motion due to the external acceleratio...
This paper analyzes the performance of an Extended Kalman Filter (EKF) based attitude estimator for...
This paper puts forward Kalman filter algorithm to improve the accuracy and the stability of four ro...
This chapter presents a complete development of a complementary filter-based attitude estimation sch...
International audienceA robust and reliable attitude estimator is a key technology enabler for the d...
AbstractUnmanned helicopters have been used extensively in the last few decades as a research platfo...