A. Awad, H. Wang. Sliding mode based integrated pitch-yaw acceleration autopilot design for varying-velocity missile. In 12th IEEE International Conference on Control and Automation, ICCA 2016, Kathmandu, Nepal, June 1-3, 2016. pages 104-109, IEEE, 2016. [doi]
@inproceedings{AwadW16,
title = {Sliding mode based integrated pitch-yaw acceleration autopilot design for varying-velocity missile},
author = {A. Awad and H. Wang},
year = {2016},
doi = {10.1109/ICCA.2016.7505260},
url = {http://dx.doi.org/10.1109/ICCA.2016.7505260},
researchr = {https://researchr.org/publication/AwadW16},
cites = {0},
citedby = {0},
pages = {104-109},
booktitle = {12th IEEE International Conference on Control and Automation, ICCA 2016, Kathmandu, Nepal, June 1-3, 2016},
publisher = {IEEE},
isbn = {978-1-5090-1738-6},
}