Robust Controller Design of Non-minimum Phase Hypersonic Aircrafts Model based on Quantitative Feedback Theory
Author:
Funder
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Link
http://link.springer.com/content/pdf/10.1007/s40295-019-00187-y.pdf
Reference35 articles.
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3. Xu, B., Shi, Z.: Universal Kirging control of hypersonic aircraft model using predictor model without back-stepping. IET Control Theory Appl. 7(4), 573–583 (2012)
4. Buschek, H., Calise, A.J.: Uncertainty modeling and fixed-order controller design for a hypersonic vehicle model. J. Guid. Control. Dyn. 20(1), 42–48 (1997)
5. Parker, J.T., Serrani, A., Yurkovich, S., Bolender, M.A., Doman, D.B.: Control-oriented modeling of an air-breathing hypersonic vehicle. J. Guid. Control. Dyn. 30(3), 856–869 (2007)
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