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Showing 1 to 7 of 7 for “"Satellite Bus"”.
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Design of a scalable nano university satellite bus (IlliniSat-2 bus) command and data handling system and power system
IlliniSat-2 bus is the second generation of a general model on which multiple-production of CubeSats are based upon. The IlliniSat-2 bus consists of Command and Data Handling system, Power Generation and Distribution system, Attitude Determination and Control system and Radio system. The …
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Use of isoperformance, constraint programming, and mixed integer linear programing for architecture tradespace exploration of passive Optical Earth Observation Systems
… uses simple algorithms to identify potential satellite bus options for hosting each sensor architecture in orbit. The total cost of populating an entire constellation based on the sensor architecture is finally estimated using cost estimates for the sensor, satellite bus, and the best launch …
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Attitude Determination and Control of Nano-Satellites
The University of Illinois's IlliniSat2 satellite bus is unique in that it is among only a few nano-satellites that implements three-axis, onboard attitude determination and control. Though this is an ambitious goal, it will allow for a wide range of scientific missions to be accomplished on this …
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Folded Lightweight Actuated Position System (FLAPS) for CubeSat Deployables
… loop as a repeatable use actuator for small satellites. SMAs are metal alloys that remember a stored shape when transitioning to the austenitic phase at a certain temperature, and are easily deformable in the martensitic phase. The transition temperature is well-defined and typically ranges …
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Contributions to the advance of the integration density of CubeSats
… is relocation of the components of multiple satellite subsystems to form a highly integrated, multi-functional solar panel. Eligible components are usually allocated to the communication system, the electric power system, or the attitude determination and control system. In a joint research …
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Modeling and Control of SPIDER Satellite Components
Space satellite technology is heading in the direction of ultra-large, lightweight structures deployable on orbit. Minimal structural mass translates into minimal launch costs, while increased satellite bus size translates into significant bandwidth improvement for both radar and optical …
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Development and testing of a modular cubeSat system enabling rapid access to space
Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2025-10-20 without embargo terms