Abstract
Based on the structured singular value synthesis of the pitch axis controller of the fighter, the standard D-K iteration algorithm was presented, the advantage of which is to ensure robustness of the system. Due to the complexity of the command-line driven D-K iteration algorithm, which is not mastered easily by control designers, the D-K iteration algorithm based on graphical user interface (GUI) was introduced, in which the whole D-K iteration procedure was integrated under a menu environment.
| Original language | English |
|---|---|
| Pages (from-to) | 742-746 |
| Number of pages | 5 |
| Journal | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| Volume | 24 |
| Issue number | 6 |
| State | Published - 1998 |
| Externally published | Yes |
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