Publisher
American Institute of Aeronautics and Astronautics
Reference21 articles.
1. Fuzzy model-based pitch stabilization and wing vibration suppression of flexible aircraft
2. Model-Predictive Gust Load Alleviation Controller for a Highly Flexible Aircraft
3. 5Reveley, M. S., Briggs, J. L., Leone, K. M., Kurtoglu, T., and Withrow, C. A., Assessment of the State of the Art of Flight Control Technologies as Applicable to Adverse Conditions, NASA Technical Report 2010216226, 2010.
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献