Review on solar sail technology

S Gong, M Macdonald - Astrodynamics, 2019 - Springer
This paper reviews solar sail trajectory design and dynamics, attitude control, and structural
dynamics. Within the area of orbital dynamics, methods relevant to transfer trajectory design …

A survey on active magnetic attitude control algorithms for small satellites

MY Ovchinnikov, DS Roldugin - Progress in Aerospace Sciences, 2019 - Elsevier
Control algorithms for the active magnetic attitude control systems are covered in the survey.
Three different situations in the magnetic system implementation are considered. First …

Design of two axes sun tracking controller with analytically solar radiation calculations

S Yilmaz, HR Ozcalik, O Dogmus, F Dincer… - … and Sustainable Energy …, 2015 - Elsevier
Photovoltaic systems have gained a great deal of interest in the world and these studies
performed on this subject have been gaining more and more importance. In order to design …

High spin rate magnetic controller for nanosatellites

A Slavinskis, U Kvell, E Kulu, I Sünter, H Kuuste, S Lätt… - Acta Astronautica, 2014 - Elsevier
This paper presents a study of a high rate closed-loop spin controller that uses only
electromagnetic coils as actuators. The controller is able to perform spin rate control and …

Chaotic attitude dynamics of a LEO satellite with flexible panels

VS Aslanov - Acta Astronautica, 2021 - Elsevier
This paper deals with the attitude motion of LEO satellites with deployable side panels
designed for passive aerodynamic stabilization in a rarefied atmosphere. The influence of …

[图书][B] Pulsed plasma thrusters for small satellites

PV Shaw - 2011 - search.proquest.com
Since the Russian launch of the Zond-2 satellite in 1964 there have been over fifty years of
research dedicated to the understanding of the first electric propulsion device to be flown in …

A novel reaction wheel unloading method with stability analysis for solar sails utilizing liquid crystal devices

H Ji, D Li - Aerospace Science and Technology, 2021 - Elsevier
Reaction wheels are capable of constituting a high-performance attitude control system for
solar sails. Unloading is significant for reaction wheels to maintain their controllability when …

Design of an aerodynamic attitude control system for a CubeSat

J Auret - 2012 - scholar.sun.ac.za
The Cape Peninsula University of Technology, in collaboration with Stellenbosch University,
is developing a 3-unit CubeSat for a low earth polar orbit. The two main payloads are a …

[PDF][PDF] Увод малых космических аппаратов с низких околоземных орбит

СП Трофимов - ИПМ им. МВ Келдыша РАН.-2G15.-126 с, 2015 - keldysh.ru
Всему свое время, и время всякой вещи под небом: время рождаться, и время умирать...
Экклезиаст, глава 3 Проблема образования космического мусора–засорения …

Three-axes attitude control of solar sail based on shape variation of booms

F Zhang, S Gong, H Baoyin - Aerospace, 2021 - mdpi.com
Actively controlling the attitude of the solar sail is necessary to adjust the solar radiation
pressure force for trajectory transfer and orbit control. The special configuration of the solar …