CubeSats are an increasingly popular platform for performing scientific research in space at a low cost. Traditional propulsive or reaction wheel based attitude control systems are complex, expensive, and require a large percentage of the nanosatellite’s volume. In this project, a low cost, low volume magnetic attitude control actuator is presented for CubeSats. The overall design is explored, with a focus on the switch mode wide dynamic range current regulator, which is built using discrete components. Results are presented, including efficiencies in excess of 95%, current set point error of less than 1%, fast and damped step responses, and output voltage ripple below 50 mV peak-to-peak. The cost and volume of the controller c...
This paper describes the development of a three axis attitude control system for nanosatellites and ...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
The goal of this report is to summarize the ideas, designs, methodologies and data of this final ye...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
This project presents the theoretical design of a magnetic actuator for use in nanosatellites, more ...
We present a satellite attitude control system design using low-cost hardware and software for a 1U ...
A miniaturized attitude control system suitable for nanosatellites, developed using only commercial ...
This paper focuses on the study and the design of an air core magnetorquer model dedicated to the 1U...
Thesis (M.S.) University of Alaska Fairbanks, 2014In recent years there has been a growing interest ...
An attitude control system (ACS) is one of the critical subsystems of any spacecraft and typically i...
This paper presents the design of an attitude controller for a magnetically actuated nanosatellite. ...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
This thesis describes the study and design of attitude control of a 1U CubeSat based on magnetorque...
In this paper, the development of a performant and accurate Attitude Determination and Control Syste...
The objective of this bachelor thesis was to display all the attitude and control systems (ACS) avai...
This paper describes the development of a three axis attitude control system for nanosatellites and ...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
The goal of this report is to summarize the ideas, designs, methodologies and data of this final ye...
International audienceThe paper deals with the attitude active control of a Low Earth Orbit nanosate...
This project presents the theoretical design of a magnetic actuator for use in nanosatellites, more ...
We present a satellite attitude control system design using low-cost hardware and software for a 1U ...
A miniaturized attitude control system suitable for nanosatellites, developed using only commercial ...
This paper focuses on the study and the design of an air core magnetorquer model dedicated to the 1U...
Thesis (M.S.) University of Alaska Fairbanks, 2014In recent years there has been a growing interest ...
An attitude control system (ACS) is one of the critical subsystems of any spacecraft and typically i...
This paper presents the design of an attitude controller for a magnetically actuated nanosatellite. ...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
This thesis describes the study and design of attitude control of a 1U CubeSat based on magnetorque...
In this paper, the development of a performant and accurate Attitude Determination and Control Syste...
The objective of this bachelor thesis was to display all the attitude and control systems (ACS) avai...
This paper describes the development of a three axis attitude control system for nanosatellites and ...
With the objective of being able to do an optic link between two CubeSats, a low cost attitude contr...
The goal of this report is to summarize the ideas, designs, methodologies and data of this final ye...