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Landing efficiency control of a six degrees of freedom aircraft model with magneto-rheological dampers: Part 2—control simulation
Journal of Intelligent Material Systems and Structures ( IF 2.7 ) Pub Date : 2020-07-23 , DOI: 10.1177/1045389x20942593 Byung-Hyuk Kang 1 , Ji-Young Yoon 1 , Gi-Woo Kim 1 , Seung-Bok Choi 1
Journal of Intelligent Material Systems and Structures ( IF 2.7 ) Pub Date : 2020-07-23 , DOI: 10.1177/1045389x20942593 Byung-Hyuk Kang 1 , Ji-Young Yoon 1 , Gi-Woo Kim 1 , Seung-Bok Choi 1
Affiliation
In Part 1 of this work, both the kinematic and dynamic equations of aircraft landing model integrated with magneto-rheological damper were derived. In Part 2, the landing efficiency is analyzed thr...
中文翻译:
具有磁流变阻尼器的六自由度飞机模型的着陆效率控制:第 2 部分——控制仿真
在本工作的第 1 部分中,推导出了集成磁流变阻尼器的飞机着陆模型的运动学和动力学方程。在第 2 部分中,着陆效率通过...
更新日期:2020-07-23
中文翻译:
具有磁流变阻尼器的六自由度飞机模型的着陆效率控制:第 2 部分——控制仿真
在本工作的第 1 部分中,推导出了集成磁流变阻尼器的飞机着陆模型的运动学和动力学方程。在第 2 部分中,着陆效率通过...