Checking the correct operation of main measuring instruments on the flight model and prototype of AIST small spacecraft
Flight model and prototype of AIST small spacecraft were launched in 2013 and 2014 respectively. They were used for carrying out various scientific researches, as well as testing the operation of AIST series small spacecrafts. They were operated in an uncontrolled flight and did not have a fullyfeat...
Main Authors: | Sedelnikov Andry, Khnyryova Ekaterina, Ivashova Tatiana |
---|---|
Format: | Article |
Language: | English |
Published: |
EDP Sciences
2018-01-01
|
Series: | MATEC Web of Conferences |
Online Access: | https://doi.org/10.1051/matecconf/201823401007 |
Similar Items
-
Method of flight operation of software and hardware for controlling parameters of the rotational motion of small spacecraft of the Aist series
by: A. V. Sedelnikov, et al.
Published: (2018-10-01) -
Thermal design of «AIST» small spacecraft
by: D. S. Kulikov, et al.
Published: (2016-04-01) -
Modal analysis of the dynamic mockup of “AIST–2D” small spacecraft
by: A. A. Igolkin, et al.
Published: (2018-07-01) -
Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft
by: N. D. Semkin, et al.
Published: (2016-12-01) -
Reduction of angular velocities of AIST-2D spacecraft using a system of kinetic moment dumping
by: M. G. Shipov
Published: (2019-07-01)