Sun-oriented attitude control is one of the most important attitude control modes for most
micro/nano satellites, which directly affects the on-orbit energy acquisition. Therefore, it is of …

View Video Presentation: https://doi. org/10.2514/6.2021-1099. vid This paper presents a
novel strategy for attitude control of a spinning spacecraft in low Earth orbit (LEO) using only …

This research relies on nutation control strategy through state feedback with its application to
a spin-stabilized autonomous system such as spacecraft. The key subject behind the …

This thesis evaluates an existing state feedback controller designed for the CubeSat MOVE-
II. In addition, the control system is further developed and a variety of control strategies are …

摘要针对低成本微小卫星的姿态控制问题, 采用无飞轮设计, 研究了在仅有磁力矩器作为控制
执行器情况下的纯磁控算法. 对多种微小卫星姿态控制算法进行了对比研究 …

A control system is designed and validated for a 3-unit CubeSat science mission. Utilizing
three magnetorquers and one reaction wheel the system achieves a 6 rotation per minute …

Lo scopo di questa tesi è quello di sviluppare e simulare diversi algoritmi per l'ACS di un
CubeSat in rotazione intorno al proprio asse di massima inerzia, con l'utilizzo di dipoli …

The purpose of this thesis is to develop and simulate different algorithms for the ACS of a
spinning CubeSat using magnetorquers and the interaction with the Earth's magnetic field …

The attitude control problem of satellite system with multiplicative noise is researched and
investigated in this paper. In order to time-varying parameters in the satellite system, the LPV …

This paper is mainly focus on the research of magnetic attitude control algorithms with only
magnetic torque based on low-cost satellites. First of all, the paper draws a comparison with …