- Paul Jackson - pjj39 (@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.
|Aastha Acharya - aa533||Christopher Atkins - ca362|
|Steven Dourmashkin - sjd227||Doug Kaiser - dtk42|
|Josh Krongelb - jnk45||Dan LaChapelle - dml337|
|William Lee - wjl57||Priya Nambiar - pkn6|
The Flight Operations team defines the detailed, on orbit operations plan for both CUSat satellites. Operating procedures are defined to match with hardware and mission specifications and help ensure successful execution of the mission.
|Alexandra Abad - mea88||Faye Elgart - fmh39|
|Kat Juraschek - kfj9||Shiva Rajagopal - svr24|
|Noah Wegener - ndw24|
The Ground Segment is responsible for the ground operations of the satellite, including ground to satellite communication, tracking and commanding.
|Arjun Biddanda - aab227||Tabatha Felter - tlf49|
|Muhammad Khan - mhk98|
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: Paul Jackson - pjj39 (@cornell.edu)