SYNTHESIS OF PROGRAM AND FINITE LAWS OF MOTION IN ANALYTICAL MODELS OF CONTROL OF THE FINAL STATE OF BIOMECHANICAL SYSTEMS

被引:2
|
作者
Zagrevskiy, V. I. [1 ,2 ]
Zagrevskiy, O. I. [2 ,3 ]
机构
[1] Mogilev State Univ, Mogilev, BELARUS
[2] Natl Res Tomsk State Univ, Tomsk, Russia
[3] Tyumen State Univ, Tyumen, Russia
来源
HUMAN SPORT MEDICINE | 2019年 / 19卷 / 01期
关键词
exercise technique; biomechanical system; control; analysis; synthesis;
D O I
10.14529/hsm190113
中图分类号
G8 [体育];
学科分类号
04 ; 0403 ;
摘要
Aim. The article deals with developing a computer program to simulate the movement of the object with a given initial and final speed and fixed travel time. Materials and methods. The analysis, as a method of biomechanics, allows us to assess the biomechanical state of the athlete in real sports exercises. The function of motion synthesis is the ability to predict the trajectory and behavior of the biomechanical system at specified reference points of the phase structure of the simulated motion. The article deals with one of the methods of biomechanical synthesis of movements: synthesis of control of the final state of biomechanical systems, based on the reduction of finite control to a given program control after attenuation of the transient component of acceleration. The mathematical description of the object motion is based on the known law of finite control with feedback. Integration of the mathematical model constructed in the form of the differential equation of the second order was carried out by one of the numerical methods of integration: Runge-Kutta method of the fourth order of accuracy. Consideration of the method is based on a mathematical apparatus describing the motion of a material point, which can be represented by a common center of mass of a biomechanical system, a joint, a center of mass of a segment, etc. Results. The mathematical model of the motion of a material point with the given kinematic parameters of motion at the initial and final moments is implemented in a computer program in the Visual Basic 2010 language environment based on the integrated development environment Visual Studio Express 2013. The output provides numerical and visual support for simulation results. Conclusion. It is shown that the developed computer model of the method always implements the goal of motion: to transfer an object from a given initial state by speed to a given final state for a fixed time of movement.
引用
收藏
页码:93 / 99
页数:7
相关论文
共 50 条
  • [1] Analytical synthesis of control laws for lateral motion of aircraft
    Zubov N.E.
    Mikrin E.A.
    Ryabchenko V.N.
    Proletarskii A.V.
    Russian Aeronautics, 2015, 58 (03): : 263 - 270
  • [2] Initial state iterative learning for final state control in motion systems
    Xu, Jian-Xin
    Huang, Deqing
    AUTOMATICA, 2008, 44 (12) : 3162 - 3169
  • [3] A FINITE STATE APPROACH TO SYNTHESIS OF BIOENGINEERING CONTROL SYSTEMS
    TOMOVIC, R
    MCGHEE, RB
    IEEE TRANSACTIONS ON HUMAN FACTORS IN ELECTRONICS, 1966, HFE7 (02): : 65 - &
  • [5] ANALYTICAL MODEL FOR COMPENSATING MOTION ERROR IN THE ADAPTIVE MOTION CONTROL OF THE BIOMECHANICAL SYSTEM
    Zagrevskiy, V. I.
    Zagrevskiy, O. I.
    HUMAN SPORT MEDICINE, 2019, 19 (02): : 79 - 85
  • [6] ADAPTIVE FINITE-STATE MODELS OF MANUAL CONTROL SYSTEMS
    ANGEL, ES
    BEKEY, GA
    IEEE TRANSACTIONS ON MAN-MACHINE SYSTEMS, 1968, MMS9 (01): : 15 - &
  • [7] Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution
    Zubov N.E.
    Mikrin E.A.
    Ryabchenko V.N.
    Fomichev A.V.
    Russian Aeronautics, 2017, 60 (1): : 64 - 73
  • [8] Synthesis of Optimal Control-Systems with a Change of the Models of Motion
    Bortakovskii, A. S.
    JOURNAL OF COMPUTER AND SYSTEMS SCIENCES INTERNATIONAL, 2018, 57 (04) : 543 - 560
  • [9] Synthesis of Optimal Control-Systems with a Change of the Models of Motion
    A. S. Bortakovskii
    Journal of Computer and Systems Sciences International, 2018, 57 : 543 - 560
  • [10] Analytical control laws of the heliocentric motion of the solar sail spacecraft
    Gorbunova, Irina
    Starinova, Olga
    10TH INTERNATIONAL CONFERENCE ON MATHEMATICAL PROBLEMS IN ENGINEERING, AEROSPACE AND SCIENCES (ICNPAA 2014), 2014, 1637 : 358 - 367