Add to ORKGAbstract: Attitude determination sensors calibration technique is presented. The sensors are composed by set of solar sensors, magnetometer and three uniaxial gyro sensors. Chibis-M small satellite attitude determination sensors have been calibrated accordingly developed technique. Calibration features are obtained for each sensor.Note: Research direction:Theoretical and applied problems of mechanic
Experimental testing of attitude determination systems still plays an important role, despite increa...
AbstractWith the fast development of nano-satellite applications, higher requirements on the method ...
Abstract: 'Chibis-M' microsatellite attitude control system is presented. Damping initial ...
International audienceContemporary information mini-satellites have general mass up to 500 kg and ar...
Attitude determination is an important subsystem of any satellite application. Several different app...
Abstract: Kalman filter study method is proposed. Application of the method is demonstrate...
In combination with magnetometers, solar sensors are one of the most used instruments for determinin...
Tools used in the measurement of satellite attitude are described. Attention is given to the element...
Attitude determination represents a fundamental task for most of the spacecrafts. It relies on three...
Abstract: Attitude determination algorithms based on Kalman filter are considered in the p...
In this report, I will discuss about the achievements and lessons learnt during this Final Year Proj...
Abstract: Star sensors BOKZ-M60 allow to find parameters that define the attitude of their...
Abstract: The problems and the design philosophy of precision autonomous gyroscopic attitude referen...
In this paper, Attitude Determination and Parameter Identification problem of a LEO satellite are st...
Magnetometers are an integral part of attitude determination system for the low-Earth orbiting small...
Experimental testing of attitude determination systems still plays an important role, despite increa...
AbstractWith the fast development of nano-satellite applications, higher requirements on the method ...
Abstract: 'Chibis-M' microsatellite attitude control system is presented. Damping initial ...
International audienceContemporary information mini-satellites have general mass up to 500 kg and ar...
Attitude determination is an important subsystem of any satellite application. Several different app...
Abstract: Kalman filter study method is proposed. Application of the method is demonstrate...
In combination with magnetometers, solar sensors are one of the most used instruments for determinin...
Tools used in the measurement of satellite attitude are described. Attention is given to the element...
Attitude determination represents a fundamental task for most of the spacecrafts. It relies on three...
Abstract: Attitude determination algorithms based on Kalman filter are considered in the p...
In this report, I will discuss about the achievements and lessons learnt during this Final Year Proj...
Abstract: Star sensors BOKZ-M60 allow to find parameters that define the attitude of their...
Abstract: The problems and the design philosophy of precision autonomous gyroscopic attitude referen...
In this paper, Attitude Determination and Parameter Identification problem of a LEO satellite are st...
Magnetometers are an integral part of attitude determination system for the low-Earth orbiting small...
Experimental testing of attitude determination systems still plays an important role, despite increa...
AbstractWith the fast development of nano-satellite applications, higher requirements on the method ...
Abstract: 'Chibis-M' microsatellite attitude control system is presented. Damping initial ...