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Triangle Interception Scenario: A Finite-Time Guidance Approach

التفاصيل البيبلوغرافية
العنوان: Triangle Interception Scenario: A Finite-Time Guidance Approach
المؤلفون: Yang Guo, Xiaoxiang Hu, Fenghua He, Hongjie Cheng, Qinhe Gao
المصدر: International Journal of Aerospace Engineering, Vol 2016 (2016)
بيانات النشر: Hindawi Limited, 2016.
سنة النشر: 2016
المجموعة: LCC:Motor vehicles. Aeronautics. Astronautics
مصطلحات موضوعية: Motor vehicles. Aeronautics. Astronautics, TL1-4050
الوصف: Considering an aircraft threatened by an interceptor, one of the effective penetration strategies is to release a Defender from the aircraft to confront the interceptor. In this case, the aircraft, the Defender, and the interceptor constitute the three-body guidance relationship, and the cooperation of the aircraft and its Defender to achieve the best tactical effects turns into a concerned problem. This paper studies the triangle interception guidance problem via the finite-time theory. The paper presents linear system Input-Output Finite-Time Stabilization (IO-FTS) method. The sufficient conditions of the linear system, being IO-FTS, under Finite-Time Boundedness (FTB) constraint are proposed, by which the state feedback controllers design method is obtained, via Linear Matrix Inequalities (LMIs). The triangle interception guidance problems are studied in three different cases, where the proposed methods are applied to the guidance design. The simulation results illustrate the effectiveness of the proposed methods.
نوع الوثيقة: article
وصف الملف: electronic resource
اللغة: English
تدمد: 1687-5966
1687-5974
Relation: https://doaj.org/toc/1687-5966; https://doaj.org/toc/1687-5974
DOI: 10.1155/2016/2942686
URL الوصول: https://doaj.org/article/185936aa9190408a906136e815bcf49c
رقم الأكسشن: edsdoj.185936aa9190408a906136e815bcf49c
قاعدة البيانات: Directory of Open Access Journals
الوصف
تدمد:16875966
16875974
DOI:10.1155/2016/2942686