Add to ORKGAbstract: The preprint presents results of the development of the first Russian nanosatellite attitude control system. The system provides an orientation of its longitudinal axis alongwith the local intensity vector of the geomagnetic field. Magnetic and geometrical parameters of the permanent magnet and hysteresis rods are calculated. Location and method of their placement are shown. Examples of transient and steady-state motion of the satellite about its centre of mass are presented.Note: Research direction:Theoretical and applied problems of mechanic
Abstract: A preprint is devoted to an orientation problem of the small axisymmetrical spin...
Abstract: Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do...
The goal of this report is to summarize the ideas, designs, methodologies and data of this final ye...
Abstract: A description of the passive magnetic attitude control system of the TNS-0 №2 na...
Abstract: The methodical and applied problems concerned the development of passive magneti...
Abstract: The first Russian nanosatellite TNS-0 was manually launched from the Internation...
Abstract: Attitude control systems which provide small satellites with a required angular ...
A passive magnetic attitude stabilization system is simple, easy to realize, cheap and does not requ...
The magnetic attitude control systems for TNS-series (Technology Nano Satellite) are considered. The...
Abstract: The methods of attitude determination of the passive magnetic stabilized nanosat...
Abstract: A problem of attitude determination of the passive magnetic stabilized nanosatel...
The objective of this bachelor thesis was to display all the attitude and control systems (ACS) avai...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
Abstract: A passive magnetic attitude control system is simple, easy to realize, low cost ...
Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do not requi...
Abstract: A preprint is devoted to an orientation problem of the small axisymmetrical spin...
Abstract: Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do...
The goal of this report is to summarize the ideas, designs, methodologies and data of this final ye...
Abstract: A description of the passive magnetic attitude control system of the TNS-0 №2 na...
Abstract: The methodical and applied problems concerned the development of passive magneti...
Abstract: The first Russian nanosatellite TNS-0 was manually launched from the Internation...
Abstract: Attitude control systems which provide small satellites with a required angular ...
A passive magnetic attitude stabilization system is simple, easy to realize, cheap and does not requ...
The magnetic attitude control systems for TNS-series (Technology Nano Satellite) are considered. The...
Abstract: The methods of attitude determination of the passive magnetic stabilized nanosat...
Abstract: A problem of attitude determination of the passive magnetic stabilized nanosatel...
The objective of this bachelor thesis was to display all the attitude and control systems (ACS) avai...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
Abstract: A passive magnetic attitude control system is simple, easy to realize, low cost ...
Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do not requi...
Abstract: A preprint is devoted to an orientation problem of the small axisymmetrical spin...
Abstract: Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do...
The goal of this report is to summarize the ideas, designs, methodologies and data of this final ye...