Advanced Search
Volume 25 Issue 5
May  1999
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 1999  >  25(5): 539-542.
Shi Peng, Li Baojun, Zhao Yushanet al. Orbital maintenance and control of spacecraft fly-around with finite-thrust[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(07): 757-760. (in Chinese)
Citation: Yang Chao, Hong Guanxin. Inflow Models in Trim and Dynamics Response of Helicopter[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(5): 539-542. (in Chinese)
shu

Inflow Models in Trim and Dynamics Response of Helicopter

  • Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 25 Mar 1998
  • Publish Date: 31 May 1999
    Abstract
  • For the current helicopter of single main rotor with tail rotor, the effect of inflow models with different characteristics on helicopter trim and digital simulation was discussed. Based on Pitt/Peters' first order dynamics nonuniform inflow model, the effect of uniform and nonuniform inflow models of main rotor on helicopter trim, and the effect of uniform and nonuniform dynamics inflow models of main rotor on helicopter dynamics response to pilot control input at different forward flight speed states, were analyzed, which could provide useful reference to chose the proper inflow model of main rotor for different flight digital simulation. The sample of UH-60A Black Hawk helicopter was used for the calculation and analysis.

     

    • FullText(HTML)
    • References(1)
  • 1. 杨 超,宋寿峰．对直升机动力学现状与发展的分析．北京航空航天大学学报, 1995, 21(2):46~52 2. 杨 超,张晓谷．直升机飞行动力学数学模型研究特点分析．飞行力学, 1998, 16(1):14~19 3. Chen R T N. A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications. Vertica, 1990, 14(2):147~184 4. Gaonkar G H, Peters D A. Review of dynamic modeling for rotorcraft flight dynamics. Vertica, 1988, 12(3):213~242 5. 包劲松, 张晓谷. 动力入流对直升机旋翼前飞操纵导数的影响. 飞行力学, 1993, 12(4):23~27 6. 杨 超．直升机飞行动力学仿射非线性系统建模与验证:[学位论文]．北京:北京航空航天大学飞行器设计与应用力学系,1995 7. 杨 超, 洪冠新, 宋寿峰. 直升机飞行动力学仿射非线性系统建模. 北京航空航天大学学报, 1997, 23(4):471~476 8. Howlett J J. UH-60A Black Hawk engineering simulation program. NASA-CR-166309, 1981
    • Relative Articles

  • Relative Articles

    [1]XU Zhiqiang, GUO Yudong, ZHANG Wenqiang, LIU Yatong, LI Ang, WANG Anni. Research on aerodynamic flow field characteristics of guide-injected icing detector[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0767
    [2]RAN Y T，PAN B F. A method for calculating reachability regions of lift re-entry vehicles with multiple constraints[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（3）：904-909 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0157.
    [3]DONG J C，GAO Q H，LIU Z H. Planar motion control of distributed-driven vehicles considering dynamic hysteresis[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3842-3853 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0887.
    [4]WANG Su, HUANG Hongdian, ZHAO Jianwen, ZHOU Hongjin, LI Qian. Master-slave AUV cooperative localization algorithm based on factor graph[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0378
    [5]CHEN Kejia, XIA Ruidong, LIN Hongxi. Textual sentiment classification incorporating dual emoji attention mechanisms[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0318
    [6]LIU H B，SHI X M，QU J B，et al. Design of Bayesian acceptance scheme for missile hit accuracy based on multinomial distribution[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1991-2000 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0516.
    [7]LI Z B，SUN W，ZHANG Y N，et al. Computation on aerodynamic and aeroacoustic characteristics of scissor tail-rotor under sideslip condition[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3794-3805 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0037.
    [8]MAO Qinghua, ZHAO Bing, LI Yang. CHAOS ephemeran algorithm combining polynomial difference learning and dimensional variation[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0698
    [9]YANG B，LIU Z，WEI X J，et al. A safety analysis approach for embedded system[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：1930-1939 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0185.
    [10]GONG K Q，WEI H K，LI J W，et al. Trajectory optimization algorithm of skipping missile based on deep reinforcement learning[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1383-1393 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0436.
    [11]HAN X，WANG Y X，CHENG X C，et al. A decentralized multi-sensor fusion estimator using finite memory buffers[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：335-343 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0240.
    [12]ZHAO G R，GU H L，HAN X，et al. NNS distributed fusion estimator under multiple network constraints[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：229-241 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0225.
    [13]ZHAO Q，FENG K. Noncontact damage imaging method in lattice sandwich structures[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（1）：206-211 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0194.
    [14]SUN Y Q，QIANG H R，DONG K H，et al. Derivation and application of iterative scheme for angle-only orbit determination[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3245-3252 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0062.
    [15]FU J W，WANG C. Configuration and multibody separation scheme of compact missile swarm[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1630-1638 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0508.
    [16]CHEN Y，CHEN J，TAO M F. Mural inpainting progressive generative adversarial networks based on structure guided[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1247-1259 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0440.
    [17]LI Yongchang, DAI Yuting, YANG Chao. Fluid and structure coupling analysis of split drag rudder[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2494-2501. doi: 10.13700/j.bh.1001-5965.2021.0151
    [18]ZHANG Zhiwen, DU Wenjie, LIANG Junfei, ZHANG Yangang, WU Yawen. Layered control of hybrid power loader based on fuel cell[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2165-2176. doi: 10.13700/j.bh.1001-5965.2021.0099
    [19]ZHENG Rao, CHEN Xiaozhu, LI Shuangxi, ZHAO Xiang, SHI Renjie, SONG Zifeng. Opening characteristics of inlaid floating ring seal with high-speed gas film[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2111-2120. doi: 10.13700/j.bh.1001-5965.2021.0083
    [20]LIU Yanbin, WANG Xuesheng, QIN Xinya, WANG Hao, CHEN Qinzhu, ZHAO Sai. Design and characteristics of reverse direct-acting high-pressure reducing valve for pneumatic actuator[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(7): 1164-1173. doi: 10.13700/j.bh.1001-5965.2021.0292
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(8094) PDF downloads(2422) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return