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AI Summary & Key Takeaways
AI Insight⚡ TL;DR(Too Long; Didn't Read)
This aircraft simulation results are very satisfactory and it has proven the validity of the developed optimal control algorithm.
📌 3 Key Takeaways
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Objective & Hypothesis:In this study, an aircraft landing problem is tested by developed optimal control algorithm.
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Key Findings & Data:The MATLAB and SIMULINK software package is used as a tool for this study.
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Conclusion & Impact:This aircraft simulation results are very satisfactory and it has proven the validity of the developed optimal control algorithm.
🔬Design:Araştırma Makalesi
📍Scope:Comprehensive Sample
⚙️Variables:Optimal kontrol · simulasyon · MATLAB
Abstract
In this study, an aircraft landing problem is tested by developed optimal control algorithm. The MATLAB and SIMULINK software package is used as a tool for this study. This aircraft simulation results are very satisfactory and it has proven the validity of the developed optimal control algorithm.
Özet
Geliştirilmiş optimal kontrol algoritması ve bu algoritmanın bir uçağın yere inmesi problemine uygulanması incelenen bu çalışmada, MATLAB ve SIMULINK software paket programı kullanılmıştır. Uçağın simülasyon sonuçları oldukça yeterlidir ve bu durum, geliştirilmiş optimal kontrol algoritmasının doğruluğunu göstermiştir.
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Cite This Article
Albostan, A., Gökbulut, M., Kekeç, A. (2013). ADAPTIVE OPTIMAL CONTROL. Gazi Üniversitesi Mühendislik Mimarlık Fakültesi Dergisi, Cilt: 11 Sayı: 1. https://ajindex.com/articles/1079244