Analysis on Hover Control Performance of T- and Cross-Shaped Tail Fin of X-Wing Single-Bar Biplane Flapping Wing
المؤلفون المشاركون
Zhu, Junru
Zhang, Pingxia
Zhu, Yongqiang
المصدر
العدد
المجلد 2020، العدد 2020 (31 ديسمبر/كانون الأول 2020)، ص ص. 1-13، 13ص.
الناشر
Hindawi Publishing Corporation
تاريخ النشر
2020-07-21
دولة النشر
مصر
عدد الصفحات
13
التخصصات الرئيسية
الملخص EN
The current flapping wing adopts T-shaped or cross-shaped tail fin to adjust its flight posture.
However, how the tail fin will affect the hover control is not very clear.
So, the effects of the two types of tail on flight will be analyzed and compared by actual flight tests in this paper.
Firstly, we proposed a new X-wing single-bar biplane flapping-wing mechanism with two pairs of wings.
Thereafter, the overall structure, gearbox structure, tail, frame, and control system of the flapping wing were designed and analyzed.
Secondly, the control mechanism of hover is analyzed to describe the effect of two-tail fin on posture control.
Thirdly, the Beetle was used as the control unit to achieve a controllable flight of flapping wing.
The MPU6050 electronic gyroscope was used to monitor the drone’s posture in real time, and the Bluetooth BLE4.0 wireless communication module was used to receive remote control instructions.
At last, to verify the flight effect, two actual flapping wings were fabricated and flight experiments were conducted.
The experiments show that the cross-shaped tail fin has a better controllable performance than the T-shaped tail fin.
The flapping wing has a high lift-to-mass ratio and good maneuverability.
The designed control system can achieve the controllable flight of the flapping wing.
نمط استشهاد جمعية علماء النفس الأمريكية (APA)
Zhang, Pingxia& Zhu, Junru& Zhu, Yongqiang. 2020. Analysis on Hover Control Performance of T- and Cross-Shaped Tail Fin of X-Wing Single-Bar Biplane Flapping Wing. Journal of Robotics،Vol. 2020, no. 2020, pp.1-13.
https://search.emarefa.net/detail/BIM-1190271
نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)
Zhang, Pingxia…[et al.]. Analysis on Hover Control Performance of T- and Cross-Shaped Tail Fin of X-Wing Single-Bar Biplane Flapping Wing. Journal of Robotics No. 2020 (2020), pp.1-13.
https://search.emarefa.net/detail/BIM-1190271
نمط استشهاد الجمعية الطبية الأمريكية (AMA)
Zhang, Pingxia& Zhu, Junru& Zhu, Yongqiang. Analysis on Hover Control Performance of T- and Cross-Shaped Tail Fin of X-Wing Single-Bar Biplane Flapping Wing. Journal of Robotics. 2020. Vol. 2020, no. 2020, pp.1-13.
https://search.emarefa.net/detail/BIM-1190271
نوع البيانات
مقالات
لغة النص
الإنجليزية
الملاحظات
Includes bibliographical references
رقم السجل
BIM-1190271
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