Finite Time Convergence Incremental Nonlinear Dynamic Inversion Based Attitude Control for Flying - Wing Aircraft with Actuator Faults

Wuhan Han, Shaojie Zhang. Finite Time Convergence Incremental Nonlinear Dynamic Inversion Based Attitude Control for Flying - Wing Aircraft with Actuator Faults. In CAA Symposium on Fault Detection, Supervision and Safety for Technical Processes, SAFEPROCESS 2019, Xiamen, China, July 5-7, 2019. pages 750-755, IEEE, 2019. [doi]

@inproceedings{HanZ19-8,
  title = {Finite Time Convergence Incremental Nonlinear Dynamic Inversion Based Attitude Control for Flying - Wing Aircraft with Actuator Faults},
  author = {Wuhan Han and Shaojie Zhang},
  year = {2019},
  doi = {10.1109/SAFEPROCESS45799.2019.9213409},
  url = {https://doi.org/10.1109/SAFEPROCESS45799.2019.9213409},
  researchr = {https://researchr.org/publication/HanZ19-8},
  cites = {0},
  citedby = {0},
  pages = {750-755},
  booktitle = {CAA Symposium on Fault Detection, Supervision and Safety for Technical Processes, SAFEPROCESS 2019, Xiamen, China, July 5-7, 2019},
  publisher = {IEEE},
  isbn = {978-1-7281-0681-6},
}