High gain observer based adaptive SMC for longitudinal dynamics of a customized mini UAV-Reference-Cited by-同舟云学术

High gain observer based adaptive SMC for longitudinal dynamics of a customized mini UAV

Published:2018 Issue: Volume: Page:
ISSN:
Container-title:Proceedings of the 2018 International Conference on Service Robotics Technologies-ICSRT '18 - ICSRT '18
language:
Short-container-title:

Author:

Hussain Sajjad¹,Malik Fahad Mumtaz¹,Altaf Omair¹,Ahmad Naseem¹

Affiliation:

1. DEE, CE&ME, National University of Sciences and Technology (NUST), Islamabad, Pakistan

Publisher

ACM Press

Reference21 articles.

1. Bronz, M., Moschetta, J., Brisset, P. and Gorraz, M. 2009. Towards a Long Endurance MAV. International Journal of Micro Air Vehicles. 1, 4 (2009), 241--254.DOI= http://journals.sagepub.com/doi/pdf/10.1260/175682909790291483.

2. Lee, D., Jin Kim, H. and Sastry, S. 2009. Feedback linearization vs. adaptive sliding mode control for a quadrotor helicopter. International Journal of Control, Automation and Systems. 7, 3 (2009), 419--428. DOI=http:// link.springer.com/article/10.1007/s12555-009-0311-8.

3. J. Huang, Y. 1993. Sliding Mode Control Design for Aircraft Control Systems. The First IEEE Regional Conference on Aerospace Control Systems. Proceedings. (1993), 309--313.

4. Magni, J., Bennani, S. and Terlouw, J. 1997. Robust Flight Control. Springer Berlin Heidelberg.

5. Zuo, Z. 2010. Trajectory tracking control design with command-filtered compensation for a quadrotor. IET Control Theory & Applications. 4, 11 (2010), 2343--2355.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Adaptive Trajectory Tracking Control for Rotorcraft Using Incremental Backstepping Sliding Mode Control Strategy;International Journal of Aerospace Engineering;2021-07-14

2. Extended-Order High-Gain Observer-Based Feedback Control Law for Tracking the Longitudinal Dynamics of a Mini UAV;Journal of Control, Automation and Electrical Systems;2019-10-24