Meeting 1

1. Why do we need stabilization after 190 minutes?

   1. Ryerson Attitude Control Systems (RACS) team has requirement

   REQ-M-PER-001

   • The spacecraft shall de-tumble within a timespan of 24 hours, it shall then autonomously switch to coarse pointing mode with magnetic torquers once the orbital estimator is operational and confirmed to be valid.

Meeting 2

1. What singularities does the tensor tech ADCS control algorithm have, if any? TODO Research
2. How robust will test verification be? Just visual checks or will we be more quantitative. If so, what other subteams will have to be involved?
3. Is MATLAB simulation of module in works?

~~TODO: Reach out to David about test harness~~

Look for reference papers for test requirements/ how helmholtz cage works in practice

Meeting 3

1. What configuration are we installing the ADCS module in
   1. If configuration 1 chosen, then GNSS doesn’t take extra space
2. How are we inputting GNSS information into the module
   1. Updated either through OBC or GNSS module
3. Does Tensor Tech Module have any singularities in Attitude Estimation Algorithm?
   1. If so → Add test cases

TODO: Write out use case for a specific test scenario in more detail. (what equipment do we need?)

Meeting 5

1. Do we have darkroom environment available? How will tests be conducted in such environment? Saw quote from tensor tech page about components required, included darkroom?
2. How to induce consistent rotation in module. Can it be done through tensor tech itself or do we need external driver?
3. Do we require a test stand to house the module on the air bearing?
   1. Some papers have designed their own test stands

Meeting 6