Based on Event-Triggered Anti-disturbance Tracking Control for Hypersonic Flight Vehicles with T-S Disturbance Modeling
Author:
Affiliation:
1. Jiangsu Aviation Technical College, China
2. Yangzhou University, China
3. University of Western Sydney, Australia
Publisher
ACM
Link
https://dl.acm.org/doi/pdf/10.1145/3483845.3483856
Reference10 articles.
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2. [ 2 ] Christopher I. Marrison Robert F. Stengel.1998.Design of robust control systems for hypersonic aircraft[J] Journal of Guidance Control and Dynamics. Vol 21 58-63.https://doi.org/10.2514/2.4197 [2] Christopher I. Marrison Robert F. Stengel.1998.Design of robust control systems for hypersonic aircraft[J] Journal of Guidance Control and Dynamics. Vol 21 58-63.https://doi.org/10.2514/2.4197
3. [ 3 ] Congcha Yao Xinmin Wang.2013.Adaptive backstepping sliding model control of hypersonic vehicle based on CMAC and dynamic surface[J] International Journal of Computer Applications in Technology.Vol 46 203-209 https://doi.org/10.1504/IJCAT.2013.052796 [3] Congcha Yao Xinmin Wang.2013.Adaptive backstepping sliding model control of hypersonic vehicle based on CMAC and dynamic surface[J] International Journal of Computer Applications in Technology.Vol 46 203-209 https://doi.org/10.1504/IJCAT.2013.052796
4. Output feedback back-stepping controlfor a generic hypersonic vehicle via small-gain theorem[J],Aerosp;Zong Qun;Sci.Technol.,2012
5. [ 5 ] Yafei Chang Tiantian Jiang Zhiqiang Pu 2017. Adaptive control of hypersonic vehicles based on characteristic models with fuzzy neural network estimators[J] Aerospace Science and Technology.Vol 68 475-485 https://doi.org/10.1016/j.ast.2017.05.043 [5] Yafei Chang Tiantian Jiang Zhiqiang Pu 2017. Adaptive control of hypersonic vehicles based on characteristic models with fuzzy neural network estimators[J] Aerospace Science and Technology.Vol 68 475-485 https://doi.org/10.1016/j.ast.2017.05.043
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1. Event-Trigger-Based Global Sliding Mode Control for a Hypersonic Morphing Vehicle;Lecture Notes in Electrical Engineering;2023
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