Library for finding the moment when a rocket has reached the highest point of its trajectory based on live altitude data.
It filters the noise with moving average and the conditions are designed to avoid false-positives which could result e.g. in opening the rocket's parachute too early.
Because it was written on AGH Space Systems workshops we only had one day to write it.
We have also created data generator to test the algorithm against noisy input with outliers.
