Results 31 to 40 of about 10,144 (241)
Providing Nanosatellite Triaxial Gravitational Orientation Using Magnetic Actuators
IOP Conference Series: Materials Science and Engineering, 2022 Three-axis gravity stabilization of 3U CubeSat is achieved due to selection of the nanosatellite moments of inertia at the design stage, as well as special modes included in the algorithm to provide stabilization of CubeSat relative to each motion ...
A. I. Leonov, P. Nikolaev
semanticscholar +1 more source
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2016 The paper presents an algorithm of damping the initial angular rate of the SamSat-218D nanosatellite after its separation from the transporting-launching container.
M. E. Melnik
doaj +1 more source
Deployment verification of large CFRP helical high-gain antenna for AIS signals [PDF]
, 2011 Deployment verification of large CFRP helical high-gain antenna for AIS ...
Baeger, Annette +4 more
core +1 more source
Design and compatibility analysis of a solar panel integrated UHF antenna for nanosatellite space mission. [PDF]
PLoS ONE, 2018 A compact UHF antenna has been presented in this paper for nanosatellite space mission. A square ground plane with slotted rectangular radiating element have been used. Coaxial probe feeding is used to excite.
Touhidul Alam +6 more
doaj +1 more source
Selection of the key earth observation sensors and platforms focusing on applications for Polar Regions in the scope of Copernicus system 2020-2030 [PDF]
, 2019 An optimal payload selection conducted in the frame of the H2020 ONION project (id 687490) is presented based on the ability to cover the observation needs of the Copernicus system in the time period 2020–2030.
Camps Carmona, Adriano José +6 more
core +2 more sources
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2019 The problem of studying thermal conditions of the optoelectronic telescopic module of a nanosatellite under the influence of operating conditions is considered. To maintain optimal thermal conditions of the telescopic lens, a thermal control system based
S. V. Tsaplin, S. A. Bolychev
doaj +1 more source
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2021 The thermal fields of the Photon-Amur 2.0 payload electronic board developed for nanosatellites were studied. The Photon-Amur 2.0 payload consists of an electronic control board with a casing mounted in a nanosatellite and a remote panel with ...
D. V. Fomin +5 more
doaj +1 more source
Mathematical model of angular motion of nanosatellites with inertial actuators
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2016 The problem of developing a nanosatellite attitude control system using three reaction wheels mounted along the main central axes of inertia is discussed in the paper. The law of controlling a nanosatellites attitude is based on a PD - controller.
M. M. Moldabekov +6 more
doaj +1 more source
Journal of the Belarusian State University. Physics, 2022 The roadmap for constructing a regional nanosatellite constellation using the piggyback launch according to Chinese provider information has developed. For nanosatellite constellation formation to a specific purpose, it is necessary to analyse existing ...
A. Spiridonov +3 more
semanticscholar +1 more source
Results of the attitude reconstruction for the UniSat-6 microsatellite using in-orbit data [PDF]
, 2016 UniSat-6 is a civilian microsatellite that was launched in orbit on the 19th of June, 2014. Its main mission consisted in the in-orbit release of a number of on-board carried Cubesats and in the transmission to the UniSat-6 ground station of telemetry ...
Chantal Cappelletti +11 more
core +3 more sources