Three-Dimensional Integrated Guidance and Control for Near Space Interceptor Based on Robust Adaptive Backstepping Approach
المؤلفون المشاركون
Gao, Changsheng
Jiang, Chunwang
Zhang, Yan
Jing, Wuxing
المصدر
International Journal of Aerospace Engineering
العدد
المجلد 2016، العدد 2016 (31 ديسمبر/كانون الأول 2016)، ص ص. 1-11، 11ص.
الناشر
Hindawi Publishing Corporation
تاريخ النشر
2016-11-24
دولة النشر
مصر
عدد الصفحات
11
الملخص EN
This study presents a novel integrated guidance and control method for near space interceptor, considering the coupling among different channels of the missile dynamics, which makes the most of the overall performance of guidance and control system.
Initially, three-dimensional integrated guidance and control model is employed by combining the interceptor-target relative motion model with the nonlinear dynamics of the interceptor, which establishes a direct relationship between the interceptor-target relative motion and the deflections of aerodynamic fins.
Subsequently, regarding the acceleration of the target as bounded uncertainty of the system, an integrated guidance and control algorithm is designed based on robust adaptive backstepping method, with the upper bound of the uncertainties unknown.
Moreover, a nonlinear tracking differentiator is introduced to reduce the “compute explosion” caused by backstepping method.
It is proved that tracking errors of the state and the upper bound of the uncertainties converge to the neighborhoods of the origin exponentially.
Finally, simulations results show that, compared to the conventional guidance and control design, the algorithm proposed in this paper has greater advantages in miss distance, required normal overload, and flight stability, especially when attacking high-maneuvering targets.
نمط استشهاد جمعية علماء النفس الأمريكية (APA)
Gao, Changsheng& Jiang, Chunwang& Zhang, Yan& Jing, Wuxing. 2016. Three-Dimensional Integrated Guidance and Control for Near Space Interceptor Based on Robust Adaptive Backstepping Approach. International Journal of Aerospace Engineering،Vol. 2016, no. 2016, pp.1-11.
https://search.emarefa.net/detail/BIM-1105014
نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)
Gao, Changsheng…[et al.]. Three-Dimensional Integrated Guidance and Control for Near Space Interceptor Based on Robust Adaptive Backstepping Approach. International Journal of Aerospace Engineering No. 2016 (2016), pp.1-11.
https://search.emarefa.net/detail/BIM-1105014
نمط استشهاد الجمعية الطبية الأمريكية (AMA)
Gao, Changsheng& Jiang, Chunwang& Zhang, Yan& Jing, Wuxing. Three-Dimensional Integrated Guidance and Control for Near Space Interceptor Based on Robust Adaptive Backstepping Approach. International Journal of Aerospace Engineering. 2016. Vol. 2016, no. 2016, pp.1-11.
https://search.emarefa.net/detail/BIM-1105014
نوع البيانات
مقالات
لغة النص
الإنجليزية
الملاحظات
Includes bibliographical references
رقم السجل
BIM-1105014
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