CN111027135B - 扑翼空气动力情况仿真方法 - Google Patents
扑翼空气动力情况仿真方法 Download PDFInfo
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CN112224440A (zh) * | 2020-10-20 | 2021-01-15 | 冯旭辉 | 一种扑翼空气动力特性高精度仿真方法 |
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CN105676672A (zh) * | 2016-01-06 | 2016-06-15 | 西北工业大学 | 扑翼飞行器复合飞行策略仿真建模方法 |
WO2017000396A1 (zh) * | 2015-06-30 | 2017-01-05 | 中国空间技术研究院 | 基于多体分析试验的桁架天线反射器展开动力学建模方法 |
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WO2017000396A1 (zh) * | 2015-06-30 | 2017-01-05 | 中国空间技术研究院 | 基于多体分析试验的桁架天线反射器展开动力学建模方法 |
CN105676672A (zh) * | 2016-01-06 | 2016-06-15 | 西北工业大学 | 扑翼飞行器复合飞行策略仿真建模方法 |
Non-Patent Citations (1)
Title |
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"基于XFlow多自由度仿鸟扑翼飞行器气动仿真";杨永刚;苏汉平;《系统仿真学报》;第30卷(第006期);2162-2167 * |
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Inventor after: Feng Zhuoqun Inventor before: Feng Zhuoqun Inventor before: Zhang Yongfei Inventor before: Chen Ke Inventor before: Meng Xiangfu Inventor before: Hu Liang |
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Effective date of registration: 20240716 Address after: Room 1004, No. 66, Lane 666, Zhuanxing Road, Minhang District, Shanghai, 201108 Patentee after: Feng Zhuoqun Country or region after: China Address before: 1555 Zhongchun Road, Minhang District, Shanghai, 201109 Patentee before: SHANGHAI AEROSPACE CONTROL TECHNOLOGY INSTITUTE Country or region before: China |