新型涵道四旋翼飞行器总体/飞控一体化设计
V275.3; 针对一种新型涵道四旋翼飞行器,提出了一种总体/飞控一体化的方案设计方法.首先,在满足设计要求的前提下,提出3种构型方案.然后,建立总体设计模型和控制模型,利用总体模型对不同构型的涵道四旋翼飞行器进行参数设计,并在控制模型中对不同状态的配平结果和不同构型的控制效果进行对比,得到评估体系.最后,对3种构型方案进行评估,确定设计方案....
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| Published in | 南京航空航天大学学报 Vol. 49; no. 2; pp. 231 - 238 |
|---|---|
| Main Authors | , |
| Format | Journal Article |
| Language | Chinese |
| Published |
南京航空航天大学直升机旋翼动力学国家级重点实验室,南京,210016
2017
|
| Subjects | |
| Online Access | Get full text |
| ISSN | 1005-2615 |
| DOI | 10.16356/j.1005-2615.2017.02.013 |
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| Abstract | V275.3; 针对一种新型涵道四旋翼飞行器,提出了一种总体/飞控一体化的方案设计方法.首先,在满足设计要求的前提下,提出3种构型方案.然后,建立总体设计模型和控制模型,利用总体模型对不同构型的涵道四旋翼飞行器进行参数设计,并在控制模型中对不同状态的配平结果和不同构型的控制效果进行对比,得到评估体系.最后,对3种构型方案进行评估,确定设计方案. |
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| AbstractList | V275.3; 针对一种新型涵道四旋翼飞行器,提出了一种总体/飞控一体化的方案设计方法.首先,在满足设计要求的前提下,提出3种构型方案.然后,建立总体设计模型和控制模型,利用总体模型对不同构型的涵道四旋翼飞行器进行参数设计,并在控制模型中对不同状态的配平结果和不同构型的控制效果进行对比,得到评估体系.最后,对3种构型方案进行评估,确定设计方案. |
| Abstract_FL | A conceptual design method of integrated general layout/flight control is presented for a new ducted quadrotor aircraft.Firstly,under the premise of meeting the design requirements,three configuration schemes for aircraft are proposed.Secondly,the overall design model and control model are established.The parametric design of ducted quadrotor aircraft with different configurations is carried out by using the overall design model,at the same time,the balancing results for different states and the control effects of different configurations schemes are compared in the control model.Then,an evaluation system is obtained.Finally,three schemes are evaluated to decide the final design. |
| Author | 范瑶 朱清华 |
| AuthorAffiliation | 南京航空航天大学直升机旋翼动力学国家级重点实验室,南京,210016 |
| AuthorAffiliation_xml | – name: 南京航空航天大学直升机旋翼动力学国家级重点实验室,南京,210016 |
| Author_FL | FAN Yao ZHU Qinghua |
| Author_FL_xml | – sequence: 1 fullname: FAN Yao – sequence: 2 fullname: ZHU Qinghua |
| Author_xml | – sequence: 1 fullname: 范瑶 – sequence: 2 fullname: 朱清华 |
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| DocumentTitle_FL | General Layout/Flight Control Integrated Design for Novel Ducted Quadrotor Aircraft |
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| Keywords | evaluation 构型方案 总体模型 控制模型 overall design model flight control model ducted quadrotor aircraft configuration design 评估 涵道四旋翼飞行器 |
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| Publisher | 南京航空航天大学直升机旋翼动力学国家级重点实验室,南京,210016 |
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| Title | 新型涵道四旋翼飞行器总体/飞控一体化设计 |
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