Abstract
Based on two performance indexes including vertical acceleration and vertical displacement of the body of civil airliner, by the nonlinear model of self-tuning of landing gear and the ARAMX model of system, using the design of controller for the multistep recursive predictor and the identification of the model parameters and system structure, the self-tuning control of landing gear was implemented. The simulation results show that the control scheme can improve the performance of taxiing for civil airliner.
| Original language | English |
|---|---|
| Pages (from-to) | 1017-1021 |
| Number of pages | 5 |
| Journal | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| Volume | 29 |
| Issue number | 11 |
| State | Published - Nov 2003 |
Keywords
- Landing gear
- Nonlinear model
- Parameter identification
- Self-tuning control
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