Code created to support a Linkedin post. Link to the original post: https://www.linkedin.com/posts/simone-bertoni-control-eng_pid-parameter-optimisation-activity ...
The proportional controller alone is not adequate to reduce the Steady State Error(SSE). It can be done with help of adding an integral controller. The basic idea is ...
Abstract: Attitude of the satellite (i.e.) its orientation about the three axis, will be of utmost importance in any satellite mission. In detumbling maneuver of a CubeSat, attitude control plays a ...
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