AbstractThe article describes nanosatellite SamSat-218D designed in Samara State Aerospace University. SamSat-218D is created for testing navigation and control technologies. The experimental on-board computer is additionally installed on the board, it have the elements of “intellectual control”. Algorithms of experimental computer are based on the principles of ensuring survivability, can detect and parry of failures of on-board elements in flight conditions
Development of small satellites has presented a great opportunity for research institutes to join sp...
This paper describes the development of a three axis attitude control system for nanosatellites and ...
Using reconfigurable and adaptable networks of micro/nanosatellites to support cost-effective space ...
AbstractThe article describes nanosatellite SamSat-218D designed in Samara State Aerospace Universit...
The goal of the research program is to develop a prototype of a satellite constellation consisting o...
AbstractAt the Samara State Aerospace University work on developing of the such nanosatellite is in ...
Recently, there has been an increased interest in using nanosatellites in space science missions due...
We have begun the feasibility study to build a small satellite in the 3kg mass range and in the powe...
Currently the GN&C’s Propulsion Branch of the NASA’s Goddard Space Flight Center (GSFC) is conductin...
Nowadays, it is widely used the term Nanosatellite when we refer to those satellites whose mass are ...
65siNanosatellites: Space and Ground Technologies, Operations and Economics comprehensively presents...
Abstract“Tian Tuo 1” (TT-1) nano-satellite is the first single-board nano-satellite that was success...
Due to their low size, mass, development cost and time, nanosatellites have become an increasingly p...
This paper describes the study and design of a 1 DoF attitude control system for a 1U CubeSat based ...
This paper introduces the three-axis attitude control of the ESAT platform. ESAT is a modular nanosa...
Development of small satellites has presented a great opportunity for research institutes to join sp...
This paper describes the development of a three axis attitude control system for nanosatellites and ...
Using reconfigurable and adaptable networks of micro/nanosatellites to support cost-effective space ...
AbstractThe article describes nanosatellite SamSat-218D designed in Samara State Aerospace Universit...
The goal of the research program is to develop a prototype of a satellite constellation consisting o...
AbstractAt the Samara State Aerospace University work on developing of the such nanosatellite is in ...
Recently, there has been an increased interest in using nanosatellites in space science missions due...
We have begun the feasibility study to build a small satellite in the 3kg mass range and in the powe...
Currently the GN&C’s Propulsion Branch of the NASA’s Goddard Space Flight Center (GSFC) is conductin...
Nowadays, it is widely used the term Nanosatellite when we refer to those satellites whose mass are ...
65siNanosatellites: Space and Ground Technologies, Operations and Economics comprehensively presents...
Abstract“Tian Tuo 1” (TT-1) nano-satellite is the first single-board nano-satellite that was success...
Due to their low size, mass, development cost and time, nanosatellites have become an increasingly p...
This paper describes the study and design of a 1 DoF attitude control system for a 1U CubeSat based ...
This paper introduces the three-axis attitude control of the ESAT platform. ESAT is a modular nanosa...
Development of small satellites has presented a great opportunity for research institutes to join sp...
This paper describes the development of a three axis attitude control system for nanosatellites and ...
Using reconfigurable and adaptable networks of micro/nanosatellites to support cost-effective space ...