To simulate the conditions of the space environment at ground, the Laboratory of Application and Innovation in Aerospace Science (LAICA) of the University of Brasília (UnB) is developing a dedicated testbed to reproducing nanosatellite attitude motion. The testbed is composed of an air-bearing table and a Helmholtz cage. The air-bearing table is a spacecraft simulator that can simulate frictionless conditions with three rotational degrees of freedom. Balancing the simulator is essential in order to make the gravitational torque negligible. The testbed is also equipped with a Helmholtz cage to recreate the Earth's magnetic field conditions that spacecrafts encounter in orbit. This paper presents the design and realization of this low-cost te...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
The paper presents a test bed designed to simulate magnetic environment experienced by a spacecraft ...
This paper describes the study and design of a 1 DoF attitude control system for a 1U CubeSat based ...
To simulate the conditions of the space environment at ground, the Laboratory of Application and Inn...
To enable a reliable verification of attitude determination and control systems for nanosatellites, ...
Due to their low size, mass, development cost and time, nanosatellites have become an increasingly p...
Growing popularity of the highly capable small- and nano-satellites, driven by components miniaturi...
In this paper we present the concept design and the progress in the realization of a spacecraft mot...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
With the surge of interest in nano-satellites, there is a concomitant need for high quality, yet aff...
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed...
In this paper, a low-cost, miniature spacecraft attitude control simulator is presented for testing ...
This paper presents the design and development of a nanosatellite-scale spacecraft three-axis simula...
This paper introduces the three-axis attitude control of the ESAT platform. ESAT is a modular nanosa...
In the last decades, access to space has become more affordable thanks to the introduction of CubeSa...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
The paper presents a test bed designed to simulate magnetic environment experienced by a spacecraft ...
This paper describes the study and design of a 1 DoF attitude control system for a 1U CubeSat based ...
To simulate the conditions of the space environment at ground, the Laboratory of Application and Inn...
To enable a reliable verification of attitude determination and control systems for nanosatellites, ...
Due to their low size, mass, development cost and time, nanosatellites have become an increasingly p...
Growing popularity of the highly capable small- and nano-satellites, driven by components miniaturi...
In this paper we present the concept design and the progress in the realization of a spacecraft mot...
Attitude control of a satellite is required for the pointing of communications antennas and other in...
With the surge of interest in nano-satellites, there is a concomitant need for high quality, yet aff...
This work describes the development of a three degrees of freedom CubeSat attitude simulator testbed...
In this paper, a low-cost, miniature spacecraft attitude control simulator is presented for testing ...
This paper presents the design and development of a nanosatellite-scale spacecraft three-axis simula...
This paper introduces the three-axis attitude control of the ESAT platform. ESAT is a modular nanosa...
In the last decades, access to space has become more affordable thanks to the introduction of CubeSa...
The validation of the Attitude Determination and Control System (ADCS) of a satellite is essential f...
The paper presents a test bed designed to simulate magnetic environment experienced by a spacecraft ...
This paper describes the study and design of a 1 DoF attitude control system for a 1U CubeSat based ...