Abstract: An algorithm for center of mass and attitude motion determination of control system mock-ups moving along the aerodynamic test-bed is proposed. The algorithms based on reference points recognition, that installed on the mock-up surface. It estimates the position, linear velocity, attitude and angular velocity of the mock-ups. The accuracy of the algorithm estimations is studied in the paper. The results of the laboratory experiments are presented.Note: Research direction:Theoretical and applied problems of mechanic
Capturing and de-orbiting space debris for removal purpose is a manoeuvre that requires the assessme...
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Once been orbited, the technological nanosatellite TNS-0 is supposed to be used in one of the next m...
Abstract: A motion control algorithm for microsatellite mock-up with flexible rods docking...
The paper proposes a two-stage algorithm for autonomous relative motion determination of noncooperat...
Abstract: Attitude and position determination algorithms based on IMU block (accelerometer...
The exceptional flight capabilities of insects have long amazed and inspired researchers and robotic...
Abstract: 'Chibis-M' microsatellite attitude control system is presented. Damping initial ...
Abstract: A description of laboratory facility developed by RDC 'ScanEx' for the microsate...
The problematics of precise pointing and more specifically an attitude control is present sincethe f...
Abstract: Kalman filter study method is proposed. Application of the method is demonstrate...
Abstract: Attitude determination algorithms based on Kalman filter are considered in the p...
Abstract: A laboratory facility developed in KIAM allows to simulate microsatellite free p...
Space science and solar system exploration are driving NASA to develop an array of small body missio...
This thesis is concerned with the motion estimation and control of Micro Aerial Vehicles (MAVs) usin...
Capturing and de-orbiting space debris for removal purpose is a manoeuvre that requires the assessme...
Relative Measurements systems represent a key technology for next generation space missions that req...
Once been orbited, the technological nanosatellite TNS-0 is supposed to be used in one of the next m...
Abstract: A motion control algorithm for microsatellite mock-up with flexible rods docking...
The paper proposes a two-stage algorithm for autonomous relative motion determination of noncooperat...
Abstract: Attitude and position determination algorithms based on IMU block (accelerometer...
The exceptional flight capabilities of insects have long amazed and inspired researchers and robotic...
Abstract: 'Chibis-M' microsatellite attitude control system is presented. Damping initial ...
Abstract: A description of laboratory facility developed by RDC 'ScanEx' for the microsate...
The problematics of precise pointing and more specifically an attitude control is present sincethe f...
Abstract: Kalman filter study method is proposed. Application of the method is demonstrate...
Abstract: Attitude determination algorithms based on Kalman filter are considered in the p...
Abstract: A laboratory facility developed in KIAM allows to simulate microsatellite free p...
Space science and solar system exploration are driving NASA to develop an array of small body missio...
This thesis is concerned with the motion estimation and control of Micro Aerial Vehicles (MAVs) usin...
Capturing and de-orbiting space debris for removal purpose is a manoeuvre that requires the assessme...
Relative Measurements systems represent a key technology for next generation space missions that req...
Once been orbited, the technological nanosatellite TNS-0 is supposed to be used in one of the next m...