Abstract
The feedforward path of an autopilot is designed for the longitudinal dynamics of a tactical missile. A linear parameter-varying model is used to synthesize a self-scheduled control law based on a parameter-dependent Lyapunov function. The controller is evaluated on a nonlinear model of industrial complexity both under nominal conditions and parametric uncertainty. Tracking performance is significantly enhanced while leaving robustness properties of an existing feedback controller unaltered.
| Original language | English (US) |
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| Title of host publication | AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015 |
| Publisher | American Institute of Aeronautics and Astronautics Inc. |
| ISBN (Electronic) | 9781510801097 |
| State | Published - 2015 |
| Event | AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015 - Kissimmee, United States Duration: Jan 5 2015 → Jan 9 2015 |
Publication series
| Name | AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015 |
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Other
| Other | AIAA Guidance, Navigation, and Control Conference 2015, MGNC 2015 - Held at the AIAA SciTech Forum 2015 |
|---|---|
| Country/Territory | United States |
| City | Kissimmee |
| Period | 1/5/15 → 1/9/15 |
Bibliographical note
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