Research on Aircraft Attitude Control Method Based on Linear Active Disturbance Rejection
In this paper, a dual-loop active disturbance rejection attitude controller design method is proposed for the attitude control of aircraft. Firstly, based on the nonlinear dynamic model of aircraft, the control system model with inner loop as angular velocity and outer loop as attitude angle is esta...
I tiakina i:
| Ngā kaituhi matua: | , , , , , |
|---|---|
| Hōputu: | Artigo |
| Reo: | Inglês |
| I whakaputaina: |
Wiley
2022-01-01
|
| Rangatū: | International Journal of Aerospace Engineering |
| Urunga tuihono: | http://dx.doi.org/10.1155/2022/1908020 |
| Ngā Tūtohu: |
Kāore He Tūtohu, Me noho koe te mea tuatahi ki te tūtohu i tēnei pūkete!
|