Aircraft Design最新文献_第2页

On-line parameter estimation for restructurable flight control systems 可重构飞行控制系统的在线参数估计

Aircraft Design Pub Date : 2001-03-01 DOI: 10.1016/S1369-8869(00)00023-9

Marcello R. Napolitano , Yongkyu Song , Brad Seanor

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引用次数: 40

Mass distribution management & dynamic balancing of aircraft mass 质量分配管理与飞机质量动态平衡

Aircraft Design Pub Date : 2001-03-01 DOI: 10.1016/S1369-8869(00)00024-0

S.M. Malaek, B. Soltan-Mohammed

{"title":"Mass distribution management & dynamic balancing of aircraft mass","authors":"S.M. Malaek, B. Soltan-Mohammed","doi":"10.1016/S1369-8869(00)00024-0","DOIUrl":"10.1016/S1369-8869(00)00024-0","url":null,"abstract":"<div><p>A new methodology has been proposed to control the distribution of mass in an aircraft during the design and development process. Having estimated the total mass, the aircraft is considered to be composed of different segments each with an unknown mass and the equations of motion are derived based on this discritized mass model. A suitable mass distribution is then found based on the desired dynamic and static stability criterion. Using this methodology the aircraft static margin can be controlled by changing the external shape (<em>X</em><sub>ac</sub>) as well as mass distribution (<em>X</em><sub>cg</sub><span>). By relating all applicable mass moments of inertia<span> to the frequencies and damping ratios<span> of longitudinal and lateral-directional dynamic modes, the chance of designing a well dynamically balanced aircraft in a variety of flight phases<span> is increased. The mathematical procedure can explicitly be derived only for rigid airplanes where two-dimensional approximations are valid. However, numerical algorithms must be used for elastic and/or rigid aircraft with coupled equations of motion. The proposed methodology has been used to find suitable mass distributions for a B-747-100 in a cruising flight while satisfying the Level-I flying quality requirements.</span></span></span></span></p></div>","PeriodicalId":100070,"journal":{"name":"Aircraft Design","volume":"4 1","pages":"Pages 51-61"},"PeriodicalIF":0.0,"publicationDate":"2001-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/S1369-8869(00)00024-0","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"76448701","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

引用次数: 3

Preliminary aircraft design: lateral handling qualities 初步飞机设计:横向操纵品质

Aircraft Design Pub Date : 2001-03-01 DOI: 10.1016/S1369-8869(00)00025-2

Paolo Teofilatto

引用次数: 3

Aircraft performance, theory and practice 飞机性能，理论与实践

Aircraft Design Pub Date : 2001-03-01 DOI: 10.1016/S1369-8869(00)00026-4

H. Wittenberg

引用次数: 0

Design of low-speed aircraft by numerical and experimental techniques developed at DPA 低速飞行器的数值与实验设计

Aircraft Design Pub Date : 2001-03-01 DOI: 10.1016/S1369-8869(00)00020-3

D.P. Coiro, F. Nicolosi

引用次数: 21

Letter to the Editor: Range and endurance of turboprop, turbofan, or piston-propeller aircraft having wings with or without camber (Ref. 3) 给编辑的信:带或不带弧形机翼的涡桨、涡扇或活塞螺旋桨飞机的航程和续航力(参考文献3)

Aircraft Design Pub Date : 2001-03-01 DOI: 10.1016/S1369-8869(00)00018-5

G.H. Berenschot

引用次数: 0

Aircraft design education in Europe 欧洲的飞机设计教育

Aircraft Design Pub Date : 2000-12-01 DOI: 10.1016/S1369-8869(00)00022-7

E Torenbeek

引用次数: 2

Aircraft design education at universities: benefits and difficulties 高校飞机设计教育:好处与困难

Aircraft Design Pub Date : 2000-12-01 DOI: 10.1016/S1369-8869(00)00014-8

Trevor M. Young

引用次数: 11

A flight dynamics course based on MATLAB computer assignments 一个基于MATLAB计算机作业的飞行动力学课程

Aircraft Design Pub Date : 2000-12-01 DOI: 10.1016/S1369-8869(00)00016-1

Lars Johansson

引用次数: 1

A proposition in design education with a potential in commercial venture in small aircraft manufacture 从事设计教育，在小型飞机制造的商业投资方面有潜力

Aircraft Design Pub Date : 2000-12-01 DOI: 10.1016/S1369-8869(00)00015-X

A.K. Kundu, S. Raghunathan

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引用次数: 5