Passification-based robust flight control design
A passification-based robust autopilot for attitude control of flexible aircraft under parametric uncertainty is designed. A high gain controller with forced sliding motions is used to secure good performance over a wide range of the aircraft model parameters. The shunting method is applied to ensur...
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| Veröffentlicht in: | Automatica (Oxford) 2011-12, Vol.47 (12), p.2743-2748 |
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| container_end_page | 2748 |
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| container_issue | 12 |
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| container_title | Automatica (Oxford) |
| container_volume | 47 |
| creator | Fradkov, Alexander L. Andrievsky, Boris |
| description | A passification-based robust autopilot for attitude control of flexible aircraft under parametric uncertainty is designed. A high gain controller with forced sliding motions is used to secure good performance over a wide range of the aircraft model parameters. The shunting method is applied to ensure closed-loop system stability under lack of aircraft state information. The series reference model is used to assign the desired closed-loop system performance. An example illustrating a typical design procedure for aircraft attitude control in the horizontal plane for different flight conditions is given. The simulation results demonstrate the efficiency and high robustness of the suggested control system. |
| doi_str_mv | 10.1016/j.automatica.2011.09.004 |
| format | Article |
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| ispartof | Automatica (Oxford), 2011-12, Vol.47 (12), p.2743-2748 |
| issn | 0005-1098 1873-2836 |
| language | eng |
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| source | Elsevier ScienceDirect Journals |
| subjects | Aircraft Attitude control Automatic pilots Automation Autopilots Computer simulation Design engineering Flight control Horizontal Passification Robustness Shunt compensation Systems stability Uncertain dynamic systems |
| title | Passification-based robust flight control design |
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