Robust Adaptive Attitude Stabilization of a Fighter Aircraft in the Presence of Input Constraints

The problem of attitude stabilization of a fighter aircraft is investigated in this paper. The practical aspects of a real physical system like existence of external disturbance with unknown upper bound and actuator saturation are considered in the process of controller design of this aircraft. In o...

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Bibliographic Details
Main Authors: M. Bahmani, T. Binazadeh
Format: Article
Language:English
Published: Shahid Rajaee Teacher Training University 2016-07-01
Series:Journal of Electrical and Computer Engineering Innovations
Subjects:
Online Access:https://jecei.sru.ac.ir/article_575_96512cbf1e3ce7d71ac7f9cd3bc8f97a.pdf