원문정보
보안공학연구지원센터(IJHIT)
International Journal of Hybrid Information Technology
Vol.4 No.1
2011.01
pp.13-24
피인용수 : 0건 (자료제공 : 네이버학술정보)
초록
영어
Wind tunnels have been used to test race cars, fighter planes etc. The hypersonic wind tunnel can hit the hypersonic speeds necessary to test the latest ultra fast aircraft and space planes. The wind tunnel is a major money saver. It allows us to make a reusable prototype and test it in the tunnel for a few hundred thousand dollars. Maintaining constant pressure in the settling chamber of the hypersonic intermittent blow down type wind tunnel is an important task for its effective performance. Here, a fuzzy assisted PI control system for the hypersonic intermittent blow down type wind tunnel is developed and analyzed.
목차
Abstract
1. Introduction
2. System model
3. PI Controller.
4. Fuzzy Assisted PI Controller.
5. Simulation Results and Discussion
6. Conclusion
7. References
1. Introduction
2. System model
3. PI Controller.
4. Fuzzy Assisted PI Controller.
5. Simulation Results and Discussion
6. Conclusion
7. References
저자정보
참고문헌
자료제공 : 네이버학술정보