A parameterized mathematical model of aircraft turning ground maneuvers

被引：0
|
作者：
机构：
[1] Yong, Tian
[2] Roca, Guillem
来源：
Yong, Tian (tianyong@nuaa.edu.cn) | 1600年 / Universidad Central de Venezuela卷 / 55期
关键词：
Friction;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [41] A Mathematical Model for Dynamic Vibration Analysis of a Landing Aircraft
    Liu, Guo-guang
    Pei, Lei-yang
    Feng, Li
    Wu, Zhi-wei
    JOURNAL OF VIBRATION ENGINEERING & TECHNOLOGIES, 2024, 12 (03) : 4149 - 4162
  • [42] A MATHEMATICAL MODEL FOR CHARGED AIRCRAFT AND ROCKETS IN AN ELECTRIC FIELD
    KASEMIR, HW
    SCHUMAN, E
    TRANSACTIONS-AMERICAN GEOPHYSICAL UNION, 1970, 51 (04): : 301 - &
  • [43] Mathematical model of one flexible transport category aircraft
    Sousa, Marcelo Santiago
    Paglione, Pedro
    Annes Silva, Roberto Gil
    Cardoso-Ribeiro, Flavio Luiz
    Cunha, Sebastiao Simoes, Jr.
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2017, 89 (03): : 384 - 396
  • [44] A MATHEMATICAL MULTIPOINT MODEL FOR AIRCRAFT MOTION IN MOVING AIR
    BROCKHAUS, R
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1987, 11 (03): : 174 - 184
  • [45] A Mathematical Model for Dynamic Vibration Analysis of a Landing Aircraft
    Guo-guang Liu
    Lei-yang Pei
    Li Feng
    Zhi-wei Wu
    Journal of Vibration Engineering & Technologies, 2024, 12 : 4149 - 4162
  • [46] Aircraft Engine Mathematical Model - Linear System Approach
    Rotaru, Constantin
    Roatesi, Simona
    Circiu, Ionica
    PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON NUMERICAL ANALYSIS AND APPLIED MATHEMATICS 2015 (ICNAAM-2015), 2016, 1738
  • [47] Mathematical Model of an Aircraft Electromechanical Actuator with Flex Coupling
    Ismagilov, F. R.
    Vavilov, V. E.
    Sayakhov, I. F.
    2017 XI INTERNATIONAL IEEE SCIENTIFIC AND TECHNICAL CONFERENCE DYNAMICS OF SYSTEMS, MECHANISMS AND MACHINES (DYNAMICS), 2017,
  • [48] MODEL OF THE OPERATOR FOR CONTROLLING THE AIRCRAFT WITH MATHEMATICAL MODELLING OF THE MOVEMENT
    Stoykov, Ognyan
    AEROSPACE RESEARCH IN BULGARIA, 2019, 31 : 143 - 149
  • [49] A Method to Calculate the Aircraft Ground Minimum Control Speed Based on Mathematical Simulation
    Huang Chengtao
    Wang Lixin
    Jia Zhongren
    2ND INTERNATIONAL SYMPOSIUM ON AIRCRAFT AIRWORTHINESS (ISAA), 2011, 17
  • [50] Mathematical modeling of helicopter aerobatic maneuvers
    Cao, YH
    Zhang, GL
    Su, Y
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2004, 76 (02): : 170 - 178
12345