Add to ORKGAbstract: A laboratory facility developed in KIAM allows to simulate microsatellite free planar motion due to aerodynamic cushion. Despite of disturbance caused by uneven surface of the table and the aerodynamic forces in the air flow free movement is not a translational straight. The determination of those distortions is presented in the paperNote: Research direction:Theoretical and applied problems of mechanic
Abstract: A description of laboratory facility developed by RDC 'ScanEx' for the microsate...
Spacecraft simulator platforms can simulate the microgravity environment of space on Earth, for the ...
Micro air vehicles (MAVs) are defined by all spatial dimensions being less than 15 cm. Equipped with...
Abstract: A description of the KIAM laboratory facility COSMOS is presented. The facility ...
grantor: University of TorontoThis thesis documents the design, build, and test, of a micr...
Abstract: An algorithm for center of mass and attitude motion determination of control sys...
Abstract: A problem of attitude simulation for SC in laboratory conditions is discussed. V...
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...
Micro-vibration is a low level disturbance, which cannot be controlled or reduced by the Attitude an...
An overview of recently completed programs in aeroelasticity and structural dynamics research at the...
grantor: University of TorontoAn experimental investigation into the stability of a flappi...
grantor: University of TorontoThe Space Shuttle middeck is an unlikely place to find a fre...
Micro rotor-craft, and micro helicopters in particular, are a class of micro aerial vehicle (MAV) th...
Micro aerial vehicles design represents a challenge that lasted for years and the fact that they ope...
Abstract: A description of laboratory facility developed by RDC 'ScanEx' for the microsate...
Spacecraft simulator platforms can simulate the microgravity environment of space on Earth, for the ...
Micro air vehicles (MAVs) are defined by all spatial dimensions being less than 15 cm. Equipped with...
Abstract: A description of the KIAM laboratory facility COSMOS is presented. The facility ...
grantor: University of TorontoThis thesis documents the design, build, and test, of a micr...
Abstract: An algorithm for center of mass and attitude motion determination of control sys...
Abstract: A problem of attitude simulation for SC in laboratory conditions is discussed. V...
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...
Micro-vibration is a low level disturbance, which cannot be controlled or reduced by the Attitude an...
An overview of recently completed programs in aeroelasticity and structural dynamics research at the...
grantor: University of TorontoAn experimental investigation into the stability of a flappi...
grantor: University of TorontoThe Space Shuttle middeck is an unlikely place to find a fre...
Micro rotor-craft, and micro helicopters in particular, are a class of micro aerial vehicle (MAV) th...
Micro aerial vehicles design represents a challenge that lasted for years and the fact that they ope...
Abstract: A description of laboratory facility developed by RDC 'ScanEx' for the microsate...
Spacecraft simulator platforms can simulate the microgravity environment of space on Earth, for the ...
Micro air vehicles (MAVs) are defined by all spatial dimensions being less than 15 cm. Equipped with...