AbstractIn micro-electro-mechanical system based inertial navigation system (MEMS-INS)/global position system (GPS) integrated navigation systems, there exist unknown disturbances and abnormal measurements. In order to obtain high estimation accuracy and enhance detection sensitivity to faults in measurements, this paper deals with the problem of model-based robust estimation (RE) and fault detection (FD). A filter gain matrix and a post-filter are designed to obtain a RE and FD algorithm with current measurements, which is different from most of the existing priori filters using measurements in one-step delay. With the designed filter gain matrix, the H-infinity norm of the transfer function from noise inputs to estimation error outputs is...
In natural and urban canyon environments, Global Navigation Satellite System (GNSS) signals suffer f...
La résolution d'un problème d'estimation de l'état d'un système nécessite de disposer d'un modèle ré...
The standard observer for inertial navigation system (INS) have for many years been the extended Kal...
In micro-electro-mechanical system based inertial navigation system (MEMS-INS)/global position syste...
error modeling. SUMMARY Integrated INS/GPS systems provide continuous positioning information in any...
Advances in the development of micro-electromechanical systems (MEMS) have made possible the fabrica...
The Global Positioning System (GPS) and an Inertial Navigation System (INS)are two basic navigation ...
ABSTRACT The performance of a GPS/INS integration system is greatly determined by the ability of sta...
The endeavours in improving the performance of a conventional non-differential GPS/MEMS IMU tightly-...
Thanks to advances in the development of Micro-Electromechanical Systems (MEMS), it has been possibl...
As an optimal estimation method, the Kalman filter is the most frequently-used data fusion strategy ...
Real-time estimation of parameters in dynamic systems becomes increasingly important in thefield of ...
Because of the sensor noises, the accuracy of a low cost INS deteriorates very rapidly with time. I...
As to an aerospace vehicle, the flight span is large and the flight environment is complex. More tha...
Due to the development of Global Navigation Satellite Systems (GNSS), multiple satellites are availa...
In natural and urban canyon environments, Global Navigation Satellite System (GNSS) signals suffer f...
La résolution d'un problème d'estimation de l'état d'un système nécessite de disposer d'un modèle ré...
The standard observer for inertial navigation system (INS) have for many years been the extended Kal...
In micro-electro-mechanical system based inertial navigation system (MEMS-INS)/global position syste...
error modeling. SUMMARY Integrated INS/GPS systems provide continuous positioning information in any...
Advances in the development of micro-electromechanical systems (MEMS) have made possible the fabrica...
The Global Positioning System (GPS) and an Inertial Navigation System (INS)are two basic navigation ...
ABSTRACT The performance of a GPS/INS integration system is greatly determined by the ability of sta...
The endeavours in improving the performance of a conventional non-differential GPS/MEMS IMU tightly-...
Thanks to advances in the development of Micro-Electromechanical Systems (MEMS), it has been possibl...
As an optimal estimation method, the Kalman filter is the most frequently-used data fusion strategy ...
Real-time estimation of parameters in dynamic systems becomes increasingly important in thefield of ...
Because of the sensor noises, the accuracy of a low cost INS deteriorates very rapidly with time. I...
As to an aerospace vehicle, the flight span is large and the flight environment is complex. More tha...
Due to the development of Global Navigation Satellite Systems (GNSS), multiple satellites are availa...
In natural and urban canyon environments, Global Navigation Satellite System (GNSS) signals suffer f...
La résolution d'un problème d'estimation de l'état d'un système nécessite de disposer d'un modèle ré...
The standard observer for inertial navigation system (INS) have for many years been the extended Kal...