The objective of this bachelor thesis was to display all the attitude and control systems (ACS) available for CubeSats and how magnetic ACS are the most convenient option in terms of volume. Precisely this project focused on the procedure, the design and the laws of physics that are behind the creation of a torque rod, a magnetic attitude and control system conceived for nanosatellites. After discussing the magnetic laws, the different types of materials of the core, and the geometric parameters of the core and of the wire, all of which determine the operating area of the system, a theoretical model for a torque rod was devised. This was done by using the models present in Niccolò Bellini’s master thesis “Magnetic actuators for nanosatell...
This paper presents the design of an attitude controller for a magnetically actuated nanosatellite. ...
An attitude control system (ACS) is one of the critical subsystems of any spacecraft and typically i...
Abstract: A problem of attitude determination of the passive magnetic stabilized nanosatel...
The goal of this report is to summarize the ideas, designs, methodologies and data of this final ye...
This project presents the theoretical design of a magnetic actuator for use in nanosatellites, more ...
Abstract: The methodical and applied problems concerned the development of passive magneti...
This paper focuses on the study and the design of an air core magnetorquer model dedicated to the 1U...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
Abstract: The preprint presents results of the development of the first Russian nanosatell...
Martynas Kisielius DESIGN AND INVESTIGATION OF VARIOUS MAGNETIC TORQUERS Summary Cubesat type of sat...
Abstract: A description of the passive magnetic attitude control system of the TNS-0 №2 na...
This thesis describes the study and design of attitude control of a 1U CubeSat based on magnetorque...
University of Minnesota M.S. thesis. January 2020. Major: Aerospace Engineering and Mechanics. Advis...
The Velox-I, developed by Nanyang Technological University, is the first Singapore build nano-satell...
The nanosatellites typically use either magnetic rods or coil to generate magnetic moment which cons...
This paper presents the design of an attitude controller for a magnetically actuated nanosatellite. ...
An attitude control system (ACS) is one of the critical subsystems of any spacecraft and typically i...
Abstract: A problem of attitude determination of the passive magnetic stabilized nanosatel...
The goal of this report is to summarize the ideas, designs, methodologies and data of this final ye...
This project presents the theoretical design of a magnetic actuator for use in nanosatellites, more ...
Abstract: The methodical and applied problems concerned the development of passive magneti...
This paper focuses on the study and the design of an air core magnetorquer model dedicated to the 1U...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
Abstract: The preprint presents results of the development of the first Russian nanosatell...
Martynas Kisielius DESIGN AND INVESTIGATION OF VARIOUS MAGNETIC TORQUERS Summary Cubesat type of sat...
Abstract: A description of the passive magnetic attitude control system of the TNS-0 №2 na...
This thesis describes the study and design of attitude control of a 1U CubeSat based on magnetorque...
University of Minnesota M.S. thesis. January 2020. Major: Aerospace Engineering and Mechanics. Advis...
The Velox-I, developed by Nanyang Technological University, is the first Singapore build nano-satell...
The nanosatellites typically use either magnetic rods or coil to generate magnetic moment which cons...
This paper presents the design of an attitude controller for a magnetically actuated nanosatellite. ...
An attitude control system (ACS) is one of the critical subsystems of any spacecraft and typically i...
Abstract: A problem of attitude determination of the passive magnetic stabilized nanosatel...