Abstract
The aerodynamic dynamic model of hovering for air vehicle with longitudinal double ducted propeller is established by analysis aerodynamic characteristics, Relative gain array of various channels is calculated to evaluate the coupling degree among various channels, Decoupling control matrix and stability augmentation control system is designed. The empirical data on scaled model shows that air vehicle could hover stably and be in good agreement with the design goal.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of 2012 International Conference on Modelling, Identification and Control, ICMIC 2012 |
| Pages | 873-877 |
| Number of pages | 5 |
| Publication status | Published - 2012 |
| Event | 2012 International Conference on Modelling, Identification and Control, ICMIC 2012 - Wuhan, China Duration: 24 Jun 2012 → 26 Jun 2012 |
Publication series
| Name | Proceedings of 2012 International Conference on Modelling, Identification and Control, ICMIC 2012 |
|---|
Conference
| Conference | 2012 International Conference on Modelling, Identification and Control, ICMIC 2012 |
|---|---|
| Country/Territory | China |
| City | Wuhan |
| Period | 24/06/12 → 26/06/12 |
Keywords
- Air Vehicle
- Decoupling Control
- Stability
Fingerprint
Dive into the research topics of 'Design of augmentation stability control system for hovering of ducted propeller air vehicle'. Together they form a unique fingerprint.Cite this
Li, M. X., Xiang, C. L., Ma, Y., Zhu, L., & Xu, B. (2012). Design of augmentation stability control system for hovering of ducted propeller air vehicle. In Proceedings of 2012 International Conference on Modelling, Identification and Control, ICMIC 2012 (pp. 873-877). Article 6260246 (Proceedings of 2012 International Conference on Modelling, Identification and Control, ICMIC 2012).