Add to ORKGAbstract: A description of the passive magnetic attitude control system of the TNS-0 №2 nanosatellite is presented. Parameters of a permanent magnet and hysteresis rods are given and their choice is justified. The results of laboratory testing of sensors installed in the satellite are shown.Note: Research direction:Theoretical and applied problems of mechanic
Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do not requi...
Abstract: Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do...
Abstract: The first Russian nanosatellite TNS-0 was manually launched from the Internation...
Abstract: The preprint presents results of the development of the first Russian nanosatell...
Abstract: The methodical and applied problems concerned the development of passive magneti...
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...
A passive magnetic attitude stabilization system is simple, easy to realize, cheap and does not requ...
A miniaturized attitude control system suitable for nanosatellites, developed using only commercial ...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
Abstract: Attitude control systems which provide small satellites with a required angular ...
The goal of this report is to summarize the ideas, designs, methodologies and data of this final ye...
Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do not requi...
Abstract: Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do...
Abstract: The first Russian nanosatellite TNS-0 was manually launched from the Internation...
Abstract: The preprint presents results of the development of the first Russian nanosatell...
Abstract: The methodical and applied problems concerned the development of passive magneti...
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...
A passive magnetic attitude stabilization system is simple, easy to realize, cheap and does not requ...
A miniaturized attitude control system suitable for nanosatellites, developed using only commercial ...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
Abstract: Attitude control systems which provide small satellites with a required angular ...
The goal of this report is to summarize the ideas, designs, methodologies and data of this final ye...
Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do not requi...
Abstract: Passive magnetic attitude stabilization systems are simple, easy to realize, cheap, and do...
Abstract: The first Russian nanosatellite TNS-0 was manually launched from the Internation...