Control of Longitudinal Flight Dynamics of a Flapping-Wing Micro Air Vehicle Using Time-Averaged Model and Differential Flatness Based Controller

Zaeem A. Khan, Sunil K. Agrawal. Control of Longitudinal Flight Dynamics of a Flapping-Wing Micro Air Vehicle Using Time-Averaged Model and Differential Flatness Based Controller. In American Control Conference, ACC 2007, New York, NY, USA, 9-13 July, 2007. pages 5284-5289, IEEE, 2007. [doi]

@inproceedings{KhanA07-2,
  title = {Control of Longitudinal Flight Dynamics of a Flapping-Wing Micro Air Vehicle Using Time-Averaged Model and Differential Flatness Based Controller},
  author = {Zaeem A. Khan and Sunil K. Agrawal},
  year = {2007},
  doi = {10.1109/ACC.2007.4283052},
  url = {https://doi.org/10.1109/ACC.2007.4283052},
  researchr = {https://researchr.org/publication/KhanA07-2},
  cites = {0},
  citedby = {0},
  pages = {5284-5289},
  booktitle = {American Control Conference, ACC 2007, New York, NY, USA, 9-13 July, 2007},
  publisher = {IEEE},
}