If we want to get some version of flight software up and running in a HOOTL environment with the new attitude controller, we'll need to make some small changes to the attitude estimator interface. Most notably, the finite difference method to determine w_body should be removed because we will be relying on filtered gyroscope measurements in the future.
Obviously, this implementation will be removed in the future.
If we want to get some version of flight software up and running in a HOOTL environment with the new attitude controller, we'll need to make some small changes to the attitude estimator interface. Most notably, the finite difference method to determine
w_bodyshould be removed because we will be relying on filtered gyroscope measurements in the future.Obviously, this implementation will be removed in the future.