Abstract
An improved method for compensator design in aircraft control applications is presented. A design technique using a pseudo-state equation together with an enlarged system is discussed. This method improves the redesign procedure when the compensator characteristics cannot meet the required specifications. The theoretical basis of the proposed method is investigated, and an algorithm is developed. To prove the effectiveness of the pseudo-state method, an example of an aircraft controller for landing approach is discussed and tested. The simulation results show that the redesign efforts are reduced, and the characteristics of the designed compensators are improved.
| Original language | English |
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| Pages | 128-133 |
| Number of pages | 6 |
| Publication status | Published - 1989 Dec 1 |
| Event | Proceedings of the 1989 American Control Conference - Pittsburgh, PA, USA Duration: 1989 Jun 21 → 1989 Jun 23 |
Other
| Other | Proceedings of the 1989 American Control Conference |
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| City | Pittsburgh, PA, USA |
| Period | 89-06-21 → 89-06-23 |
All Science Journal Classification (ASJC) codes
- Engineering(all)