Below are the input and output data for the applications in the paper "Computing Dynamic Output Feedback Laws".

  1. Satellite Trajectory Control   

 

  1. Numerical Example A

 

  1. Numerical Example B

 

  1. Aircraft Control   

This material is based upon work supported by the National Science Foundation under Grants No. 0105739, and 0134611. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the author(s) and do not necessarily reflect the views of the National Science Foundation.