Abstract
A controller is designed by establishing the nonlinear model and the ARMAX model of system for the self-tuning of landing gear. The self-tuning control is realized in combination with parameter identification. The simulation results show that the control scheme can improve the absorber capability of landing gear.
| Original language | English |
|---|---|
| Pages (from-to) | 237-241 |
| Number of pages | 5 |
| Journal | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
| Volume | 25 |
| Issue number | 3 |
| State | Published - May 2004 |
Keywords
- Landing gear
- Non-linear model
- Parameter identification
- Self-tuning control
- Taxiing load
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