Closed Loop Analysis of Space Systems (CLASS) is a small satellite test system engineered and maintained by the Laboratory for Advanced Space Systems at Illinois (LASSI), which is affiliated with the Department of Aerospace Engineering at the University of Illinois at Urbana-Champaign. CLASS is designed to be modular and user-friendly while providing the capability to perform accurate and reliable closed-loop tests. Commercial and academic CubeSat developers struggle to implement adequate testing procedures because of the relatively short development timeline and the sophisticated and inaccessible nature of space systems test equipment. Hardware-in-the-loop testing offers a convenient “test-as-you-fly, fly-as-you-test” validation and verifi...
The University of Illinois has developed the IlliniSat-2 CubeSat bus, a generic scalable and modular...
Low Earth Orbit is becoming an inexpensive and readily available technology demonstration environmen...
A cubesat attitude control system (ACS) was designed at the NASA Marshall Space Flight Center (MSFC)...
Closed Loop Analysis of Space Systems (CLASS) is a modular, closed-loop satellite test system develo...
The attitude determination and control system (ADCS) for a satellite is responsible for multiple key...
Since their creation in 1999, CubeSats have quickly erupted into a worldwide phenomenon. With missio...
Over the last year, Cal Poly Pomona has made a significant push to become a consistent space-faring ...
Space systems are notoriously difficult to develop due to the nature of the environment in which the...
The paper describes the Hardware-In-the-Loop (HIL) simulation methodology used in the development of...
There are multiple common reasons for CubeSats’ failure. These include power, mechanical, and commun...
The problem of testing the performance of an attitude control system presents new challenges and opp...
Using CubeSat/nanosat missions as technology demonstrators requires minimizing sources of potential ...
The paper presents an end-to-end simulator aimed at supporting the engineering team in the design an...
The importance of small satellites, and in particular of nano-satellites (e.g. CubeSats) has increas...
This research endeavors to evaluate and characterize the performance of CubeSat specific commercial-...
The University of Illinois has developed the IlliniSat-2 CubeSat bus, a generic scalable and modular...
Low Earth Orbit is becoming an inexpensive and readily available technology demonstration environmen...
A cubesat attitude control system (ACS) was designed at the NASA Marshall Space Flight Center (MSFC)...
Closed Loop Analysis of Space Systems (CLASS) is a modular, closed-loop satellite test system develo...
The attitude determination and control system (ADCS) for a satellite is responsible for multiple key...
Since their creation in 1999, CubeSats have quickly erupted into a worldwide phenomenon. With missio...
Over the last year, Cal Poly Pomona has made a significant push to become a consistent space-faring ...
Space systems are notoriously difficult to develop due to the nature of the environment in which the...
The paper describes the Hardware-In-the-Loop (HIL) simulation methodology used in the development of...
There are multiple common reasons for CubeSats’ failure. These include power, mechanical, and commun...
The problem of testing the performance of an attitude control system presents new challenges and opp...
Using CubeSat/nanosat missions as technology demonstrators requires minimizing sources of potential ...
The paper presents an end-to-end simulator aimed at supporting the engineering team in the design an...
The importance of small satellites, and in particular of nano-satellites (e.g. CubeSats) has increas...
This research endeavors to evaluate and characterize the performance of CubeSat specific commercial-...
The University of Illinois has developed the IlliniSat-2 CubeSat bus, a generic scalable and modular...
Low Earth Orbit is becoming an inexpensive and readily available technology demonstration environmen...
A cubesat attitude control system (ACS) was designed at the NASA Marshall Space Flight Center (MSFC)...