Dynamics Modeling and Simulation of Circularly Aerial Towed Cable Systems
CSTR:
Author:
Clc Number:

V243

  • Article
  • | |
  • Metrics
  • |
  • Reference [14]
  • |
  • Related [20]
  • | | |
  • Comments
    Abstract:

    The multi-body dynamics model of the towed cable is proposed in the aircraft circular motion. Based on the analysis of motion state and force of the towed cable which is established via the multi-rigid method, the dynamic simulation analysis is carried out, and the steady configuration of the rotation balance is achieved. In the same condition, it is similar to the numerical calculation configuration of micro-element method of the continuous model. All these illustrate that the new dynamic model is correct and credible, and the simulation solution is also robust and accurate. Finally, the influence of various parameters on the vertical length of the towed cable is analyzed in detail. The simulation results show that the aircraft speed is the most important factor which affects the system’s efficiency, and with some certain conditions, reasonable reducing the aircraft speed can increase the vertical length of the towed cable. The effective speed range is also calculated by the dichotomy.

    Reference
    [1] 李红泉. 新型航空拖缆制作与检测方法[J]. 兵工自动化,2014, 33(5): 19-21.LI Hongquan. Manufacture and test method for a new towing cable[J]. Ordnance Industry Automation, 2014, 33(5): 19-21.
    [2] 韩维,侯志强.机载拖曳系统的建模和若干动力学问题[C]. 中国2005年飞行力学与飞行实验学术年会论文集. 西安:飞行力学杂志社,2005: 1-5.HAN Wei, HOU Zhiqiang. The modeling and some dynamic problem of the trailing cable on an aircraft[C]. The Flight Dynamic and Flight Experimentation Conference of China. Xi’ an: The Flight Dynamic Press, 2005: 1-5.
    [3] Caughey T K. Whirling of a Heavy Chain[C]. Proceedings of the 3rd U.S. National Congress of Applied Mechanics, American Society of Mechanical Engineers, New York, 1958.
    [4] Lemon G, Fraser W B. Steady-State Bifurcations and Dynamical Stability of a Heavy Whirling Cable Acted on by Aerodynamic Drag[J]. Proceedings of the Royal Society of London A, 2001, 457: 1021–1041.
    [5] Skop R A, Choo Y I. The Configuration of a Cable Towed in a Circular Path[J]. Journal of Aircraft, 1971, 8(11): 856–862.
    [6] Huang S L. Mathematical model for long cable by orbiting aircraft[R]. Johnsville, Pa. : Naval Air Development Center, 1969.
    [7] Zhu F, Rahn C D. Stability analysis of a circularly towed cable-body system[J]. Journal of Sound and Vibration, 1998, 217(3): 435-452.
    [8] 郑小洪,韩维,贾忠湖,等. 机载拖曳天线动力学建模与仿真[J]. 飞行力学,2013, 31(3): 234-238.ZHENG Xiaohong, HAN Wei, JIA Zhonghu, et al. Dynamic modeling and simulation of airborne trailing antenna[J]. Flight Dynamics, 2013, 31(3): 234-238.
    [9] Choo Y, Casarella M J. A Survey of Analytical Methods for Dynamic Simulation of Cable-Body Systems[J]. Journal of Hydronautics, 1973, 7(4): 137-142.
    [10] Russell J J, Anderson W J. Equilibrium and Stability of a Whirling Rod-Mass System[J]. International Journal of Non-Linear Mechanics, 1977, 12(2): 91–101.
    [11] James M C, Dr Louis V S. Dynamic modeling of a trailing wire towed by an orbiting aircraft [R]. AIAA-93-3663-CP, 1993.
    [12] Paul W, Pavel T. A study on the transitional dynamics of a towed-circular aerial cable system[C]//AIAA Atmospheric Flight Mechanics Conference and Exhibit. San Francisco, California, American Institute of Aeronautics and Astronautics, 2005.
    [13] Hoerner S F. Fluid Dynamic Drag[M]. 1965, Chap. 3.
    [14] Johnny E Q, Andrew S A. Dynamic Simulation of Low Altitude Aerial Tow Systems[C]. AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2004.
    Cited by
    Comments
    Comments
    分享到微博
    Submit
Get Citation

ZHU Yanjuan, LUO Dan. Dynamics Modeling and Simulation of Circularly Aerial Towed Cable Systems[J].同济大学学报(自然科学版),2018,46(01):0081~0086

Copy
Share
Article Metrics
  • Abstract:1287
  • PDF: 1091
  • HTML: 578
  • Cited by: 0
History
  • Received:July 19,2017
  • Revised:November 21,2017
  • Adopted:October 09,2017
  • Online: February 01,2018
Article QR Code