Abstract
In this paper dynamic inversion and structured singular value (μ) techniques are applied to the design of lateral/directional controllers for a high performance aircraft. The controllers are designed to achieve specified handling qualities with robustness to modeling errors.
| Original language | English (US) |
|---|---|
| Title of host publication | Guidance, Navigation, and Control Conference |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| Pages | 738-749 |
| Number of pages | 12 |
| State | Published - Jan 1 1995 |
| Event | Guidance, Navigation, and Control Conference, 1995 - Baltimore, United States Duration: Aug 7 1995 → Aug 10 1995 |
Other
| Other | Guidance, Navigation, and Control Conference, 1995 |
|---|---|
| Country/Territory | United States |
| City | Baltimore |
| Period | 8/7/95 → 8/10/95 |