Adaptive Fuzzy Control for Attitude Stabilization of Spacecraft with Deployable Composite Laminated Solar Array
المؤلفون المشاركون
Zhang, Wei
Zhu, Weibing
Zhang, Shijie
Zhao, Xiangtian
المصدر
العدد
المجلد 2020، العدد 2020 (31 ديسمبر/كانون الأول 2020)، ص ص. 1-26، 26ص.
الناشر
Hindawi Publishing Corporation
تاريخ النشر
2020-08-04
دولة النشر
مصر
عدد الصفحات
26
التخصصات الرئيسية
الملخص EN
Modern spacecraft are often equipped with large-scale, complex, and lightweight solar arrays whose deployment involves a highly dynamic movement.
This paper proposed a novel adaptive proportional-derivative typed fuzzy logic control scheme for the attitude stabilization of a flexible spacecraft during the deployment of a composite laminated solar array.
First, a constrained rigid-flexible coupling spacecraft model consisting of a rigid main body and a flexible solar array was proposed.
The solar array, which is composed of composite laminated shells, was described by the absolute nodal coordinate formulation.
Then, the detailed derivation of the adaptive fuzzy PD controller for attitude stabilization of the spacecraft was discussed.
In addition, the spacecraft dynamic model which integrated the adaptive fuzzy PD controller was derived as a set of differential-algebraic equations.
Several simulations were developed to investigate the solar array deployment dynamics and to verify the effectiveness of the proposed adaptive fuzzy PD controller.
The results suggested that the proposed dynamic model is able to exactly describe the deployment dynamics of the composite laminated solar array.
The solar array deployment causes obvious translational and rotational motions of the spacecraft.
The proposed adaptive fuzzy PD control scheme has better performance in terms of the control precision and time response in stabilizing spacecraft during the deployment of the composite laminated solar array, comparing with that of the conventional PD controller.
نمط استشهاد جمعية علماء النفس الأمريكية (APA)
Zhang, Wei& Zhu, Weibing& Zhang, Shijie& Zhao, Xiangtian. 2020. Adaptive Fuzzy Control for Attitude Stabilization of Spacecraft with Deployable Composite Laminated Solar Array. Complexity،Vol. 2020, no. 2020, pp.1-26.
https://search.emarefa.net/detail/BIM-1141292
نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)
Zhang, Wei…[et al.]. Adaptive Fuzzy Control for Attitude Stabilization of Spacecraft with Deployable Composite Laminated Solar Array. Complexity No. 2020 (2020), pp.1-26.
https://search.emarefa.net/detail/BIM-1141292
نمط استشهاد الجمعية الطبية الأمريكية (AMA)
Zhang, Wei& Zhu, Weibing& Zhang, Shijie& Zhao, Xiangtian. Adaptive Fuzzy Control for Attitude Stabilization of Spacecraft with Deployable Composite Laminated Solar Array. Complexity. 2020. Vol. 2020, no. 2020, pp.1-26.
https://search.emarefa.net/detail/BIM-1141292
نوع البيانات
مقالات
لغة النص
الإنجليزية
الملاحظات
Includes bibliographical references
رقم السجل
BIM-1141292
قاعدة معامل التأثير والاستشهادات المرجعية العربي "ارسيف Arcif"
أضخم قاعدة بيانات عربية للاستشهادات المرجعية للمجلات العلمية المحكمة الصادرة في العالم العربي
تقوم هذه الخدمة بالتحقق من التشابه أو الانتحال في الأبحاث والمقالات العلمية والأطروحات الجامعية والكتب والأبحاث باللغة العربية، وتحديد درجة التشابه أو أصالة الأعمال البحثية وحماية ملكيتها الفكرية. تعرف اكثر