Attitude Optimal Backstepping Controller Based Quaternion for a UAV

المؤلفون المشاركون

Djamel, Kaddouri
Abdellah, Mokhtari
Benallegue, Abdelaziz

المصدر

Mathematical Problems in Engineering

العدد

المجلد 2016، العدد 2016 (31 ديسمبر/كانون الأول 2016)، ص ص. 1-11، 11ص.

الناشر

Hindawi Publishing Corporation

تاريخ النشر

2016-03-03

دولة النشر

مصر

عدد الصفحات

11

التخصصات الرئيسية

هندسة مدنية

الملخص EN

A hierarchical controller design based on nonlinear H∞ theory and backstepping technique is developed for a nonlinear and coupled dynamic attitude system using conventional quaternion based method.

The derived controller combines the attractive features of H∞ optimal controller and the advantages of the backstepping technique leading to a control law which avoids winding phenomena.

Performance issues of the controller are illustrated in a simulation study made for a four-rotor vertical take-off and landing (VTOL) aerial robot prototype known as the quadrotor aircraft.

نمط استشهاد جمعية علماء النفس الأمريكية (APA)

Djamel, Kaddouri& Abdellah, Mokhtari& Benallegue, Abdelaziz. 2016. Attitude Optimal Backstepping Controller Based Quaternion for a UAV. Mathematical Problems in Engineering،Vol. 2016, no. 2016, pp.1-11.
https://search.emarefa.net/detail/BIM-1112736

نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)

Djamel, Kaddouri…[et al.]. Attitude Optimal Backstepping Controller Based Quaternion for a UAV. Mathematical Problems in Engineering No. 2016 (2016), pp.1-11.
https://search.emarefa.net/detail/BIM-1112736

نمط استشهاد الجمعية الطبية الأمريكية (AMA)

Djamel, Kaddouri& Abdellah, Mokhtari& Benallegue, Abdelaziz. Attitude Optimal Backstepping Controller Based Quaternion for a UAV. Mathematical Problems in Engineering. 2016. Vol. 2016, no. 2016, pp.1-11.
https://search.emarefa.net/detail/BIM-1112736

نوع البيانات

مقالات

لغة النص

الإنجليزية

الملاحظات

Includes bibliographical references

رقم السجل

BIM-1112736