Adaptive Backlash Compensation Method Based on Touch State Observation for a Solid Ducted Rocket
المؤلفون المشاركون
Wang, An
Zeng, Qinghua
Ma, Likun
Wang, Hongfu
المصدر
International Journal of Aerospace Engineering
العدد
المجلد 2020، العدد 2020 (31 ديسمبر/كانون الأول 2020)، ص ص. 1-12، 12ص.
الناشر
Hindawi Publishing Corporation
تاريخ النشر
2020-11-18
دولة النشر
مصر
عدد الصفحات
12
الملخص EN
A hysteresis model was built to describe the backlash of the flow regulator in a solid ducted rocket, and its influence on the engine control was also analyzed in this study.
An adaptive backlash compensation method was proposed under two challenges: limited information and backlash state variation caused by the harsh environment in the gas generator.
The touch state is designed and its observation is used to get the state of backlash, and a compensation control method using the existing information was carried out combined with the motion intention.
This method greatly shortened the time during the transition and reduced the hysteresis effect on the control system.
Furthermore, the compensation method is improved and acquires a self-learning ability, the compensation parameter changes adaptively during the process of flow regulation, and it is able to meet the challenge of an unknown and variable state of backlash.
Finally, the validation of the compensation method was carried out with two simulations.
نمط استشهاد جمعية علماء النفس الأمريكية (APA)
Wang, An& Zeng, Qinghua& Ma, Likun& Wang, Hongfu. 2020. Adaptive Backlash Compensation Method Based on Touch State Observation for a Solid Ducted Rocket. International Journal of Aerospace Engineering،Vol. 2020, no. 2020, pp.1-12.
https://search.emarefa.net/detail/BIM-1168155
نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)
Wang, An…[et al.]. Adaptive Backlash Compensation Method Based on Touch State Observation for a Solid Ducted Rocket. International Journal of Aerospace Engineering No. 2020 (2020), pp.1-12.
https://search.emarefa.net/detail/BIM-1168155
نمط استشهاد الجمعية الطبية الأمريكية (AMA)
Wang, An& Zeng, Qinghua& Ma, Likun& Wang, Hongfu. Adaptive Backlash Compensation Method Based on Touch State Observation for a Solid Ducted Rocket. International Journal of Aerospace Engineering. 2020. Vol. 2020, no. 2020, pp.1-12.
https://search.emarefa.net/detail/BIM-1168155
نوع البيانات
مقالات
لغة النص
الإنجليزية
الملاحظات
Includes bibliographical references
رقم السجل
BIM-1168155
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