- Tricia Hevers - teh32 (@cornell.edu)
- Dr. Mark Campbell
- Dr. Mark Psiaki
- Liran Gazit - lg345
The Attitude Determination, Control, and Navigation Subsystem (ADCNS) executes the relative navigation that will be used for CUSat's in-orbit inspection procedures. CUSat will primarily be using three GPS boards for attitude determination. For attitude control, CUSat will be using pulsed-plasma thrusters (PPTs) and torque coils. The software portion of ADCNS will consist of the relative navigation algorithms, which will run the various modes of operation defined by the CONOPs.
|Samiul Nur - shn23||Shuyan Qin - sq35|
|Kantaphat Sirison - ms2285||David Song - dys23|
The CUSat Satellite project employs Systems Engineering extensively. The Systems group is largely responsible for providing the project with direction by creating top level system requirements, creating best practices, maintaining communications, making design choices, and creating processes for creating a successful product. Each of the subsystem leads also participates as a member of the Systems group, which allows the project to maintain consistency and focus.
Lead: Tricia Hevers - teh32 (@cornell.edu)