Closed Loop Analysis of Space Systems (CLASS) is a modular, closed-loop satellite test system developed at the Laboratory for Advanced Space Systems at Illinois (LASSI). This thesis presents the technical details of the initial engineering development stages of CLASS. The CubeSat concept is now twenty-one years old, yet a significantly high number of mission failures (i.e., 33% for commercial developers and 55% for academic developers) are still being experienced. By employing hardware-in-the-loop testing driven by closed-loop simulations, critical aspects of validation and verification can be achieved with improved fidelity in an attempt to enhance the mission success rate of CubeSats. CLASS is composed of real-time satellite orbital mecha...
This project handled the design and analysis of the attitude determination and control, command and ...
Since their creation, CubeSats have become a valuable educational tool for university science and en...
textA flexible, robust attitude determination and control (ADC) system is presented for small satell...
Closed Loop Analysis of Space Systems (CLASS) is a small satellite test system engineered and mainta...
Since their creation in 1999, CubeSats have quickly erupted into a worldwide phenomenon. With missio...
Space systems are notoriously difficult to develop due to the nature of the environment in which the...
textAn autonomous mission manager is being developed for use on CubeSats to perform proximity operat...
The paper describes the Hardware-In-the-Loop (HIL) simulation methodology used in the development of...
Over the last year, Cal Poly Pomona has made a significant push to become a consistent space-faring ...
The paper presents an end-to-end simulator aimed at supporting the engineering team in the design an...
The University of Illinois has developed the IlliniSat-2 CubeSat bus, a generic scalable and modular...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
The attitude determination and control system (ADCS) for a satellite is responsible for multiple key...
This paper describes the simulator technology and the verification campaign for the e-st@r CubeSats ...
This paper describes the Hardware-In-the-Loop (HIL) simulation methodology used for the verification...
This project handled the design and analysis of the attitude determination and control, command and ...
Since their creation, CubeSats have become a valuable educational tool for university science and en...
textA flexible, robust attitude determination and control (ADC) system is presented for small satell...
Closed Loop Analysis of Space Systems (CLASS) is a small satellite test system engineered and mainta...
Since their creation in 1999, CubeSats have quickly erupted into a worldwide phenomenon. With missio...
Space systems are notoriously difficult to develop due to the nature of the environment in which the...
textAn autonomous mission manager is being developed for use on CubeSats to perform proximity operat...
The paper describes the Hardware-In-the-Loop (HIL) simulation methodology used in the development of...
Over the last year, Cal Poly Pomona has made a significant push to become a consistent space-faring ...
The paper presents an end-to-end simulator aimed at supporting the engineering team in the design an...
The University of Illinois has developed the IlliniSat-2 CubeSat bus, a generic scalable and modular...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
The attitude determination and control system (ADCS) for a satellite is responsible for multiple key...
This paper describes the simulator technology and the verification campaign for the e-st@r CubeSats ...
This paper describes the Hardware-In-the-Loop (HIL) simulation methodology used for the verification...
This project handled the design and analysis of the attitude determination and control, command and ...
Since their creation, CubeSats have become a valuable educational tool for university science and en...
textA flexible, robust attitude determination and control (ADC) system is presented for small satell...