( en | de | ru )

 

Disambiguation of "Lu, Kunfeng"

Author of the publication

copydeleteadd this publication to your clipboard
Robust H∞ control for uncertain delta system with time delays and non-linear perturbations based on delta operators approach.

, , , and . Int. J. Model. Identif. Control., 11 (3/4): 150-163 (2010)

Please choose a person to relate this publication to

To differ between persons with the same name, the academic degree and the title of an important publication will be displayed. You can also use the button next to the name to display some publications already assigned to the person.

Lu Lu

Jing Lu

Lu Zhang

Qianhao Lu

Yanfeng Lu

 

Other publications of authors with the same name

Data-Driven Model-Free Adaptive Attitude Control Approach for Launch Vehicle With Virtual Reference Feedback Parameters Tuning Method., , , , and . IEEE Access, (2019)Robust passive for uncertain Markovian jump system with mode-dependent time delays., , , and . Int. J. Model. Identif. Control., 11 (3/4): 138-149 (2010)Centralized Fusion Based on Interacting Multiple Model and Adaptive Kalman Filter for Target Tracking in Underwater Acoustic Sensor Networks., , , , , , and . IEEE Access, (2019)Active attitude fault-tolerant tracking control of flexible spacecraft via the Chebyshev neural network., , and . Trans. Inst. Meas. Control, 41 (4): 925-933 (2019)Adaptive fuzzy finite-time fault-tolerant attitude control of rigid spacecraft., , , and . J. Frankl. Inst., 352 (10): 4225-4246 (2015)Robust H∞ control for uncertain delta system with time delays and non-linear perturbations based on delta operators approach., , , and . Int. J. Model. Identif. Control., 11 (3/4): 150-163 (2010)Decentralised finite-time attitude synchronisation and tracking control for rigid spacecraft., , , and . Int. J. Systems Science, 46 (14): 2493-2509 (2015)Controller design for rigid spacecraft attitude tracking with actuator saturation., , and . Inf. Sci., (2013)Asynchronous Multirate Multisensor Data Fusion Over Unreliable Measurements With Correlated Noise., , , , , and . IEEE Trans. Aerosp. Electron. Syst., 53 (5): 2427-2437 (2017)Finite-time fault tolerant control for spacecraft using sliding mode method., , , and . IECON, page 6516-6520. IEEE, (2017)