Measuring and solving real coning motion of spinning carriers

被引:4
|
作者
Zhang, Shuangbiao [1 ,2 ,3 ]
Li, Xingcheng [1 ,2 ]
Su, Zhong [3 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, 5 South Zhongguancun St, Beijing 100081, Peoples R China
[2] Minist Educ, Key Lab Dynam & Control Flight Vehicle, Beijing, Peoples R China
[3] Beijing Informat Sci & Technol Univ, Beijing Key Lab High Dynam Nav Technol, Beijing, Peoples R China
基金
中国国家自然科学基金;
关键词
Coning motion; spinning carriers; inertial measurement; circular motion; high dynamic; STABILITY; COMPENSATION; AUTOPILOT; MISSILES;
D O I
10.1177/0954410015624720
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Coning motion of spinning carriers is a complex rotating motion with various forms that include single circular motion, double circular motion and multiple circular motion. Due to the fact that it is difficult to describe the real coning motion of double circular motion and multiple circular motion by the common method of attack angle and sideslip angle (A-S), a cone frame and cone angles are defined to describe coning motion. Through analysis of measuring the relationship between coning motion and inertial devices such as gyroscopes and accelerometers, an inertial measuring method is proposed to build the measuring equation and resolving equation. A geometry-solving algorithm of real coning motion is derived in detail, and radiuses of large circle and real cone circle are obtained as well. A flight simulation of a spinning carrier with coning motion is designed and used to verify the measuring method and the geometry-solving algorithm. The result shows that: (1) the inertial measuring method has the same validity as A-S method to describe coning motion, but is superior to A-S method for the reason of providing the rotation information of carriers; (2) due to coupling relationship, the rotating angle is equal to the subtraction of roll angle and precession angle; (3) the real precession angle and the real nutation angle are calculated by the geometry-solving algorithm, and the real coning motion is obtained finally.
引用
下载
收藏
页码:2369 / 2378
页数:10
相关论文
共 50 条
  • [21] Dynamical Modeling and Hopf Bifurcation for the Coning Motion of Spinning Missiles under Single-Channel Control
    Xu Y.-L.
    Yue B.-Z.
    Zhao L.-Y.
    Yuhang Xuebao/Journal of Astronautics, 2020, 41 (04): : 398 - 409
  • [22] Coning instability analysis of spinning solid rocket motor
    Gao, Ye
    Yang, Dan
    Xiong, Yong-Liang
    Yuhang Xuebao/Journal of Astronautics, 2008, 29 (01): : 270 - 275
  • [23] Active Coning Compensation for Control of Spinning Flying Vehicles
    Salman, Mishah Uzziel
    Chang, Borchin
    2010 IEEE INTERNATIONAL CONFERENCE ON CONTROL APPLICATIONS, 2010, : 1832 - 1837
  • [24] AERODYNAMICS OF BODIES OF REVOLUTION IN CONING MOTION
    TOBAK, M
    SCHIFF, LB
    PETERSON, VL
    AIAA JOURNAL, 1969, 7 (01) : 95 - &
  • [25] The coning motion stability analysis of rocket
    Wang, Hua-Bi
    Wu, Jia-Sheng
    Binggong Xuebao/Acta Armamentarii, 2008, 29 (05): : 562 - 566
  • [26] NONLINEAR AERODYNAMICS OF BODIES IN CONING MOTION
    SCHIFF, LB
    AIAA JOURNAL, 1972, 10 (11) : 1517 - &
  • [27] MOMENT EXERTED ON A CONING PROJECTILE BY A SPINNING LIQUID IN A SPHEROIDAL CAVITY
    MURPHY, CH
    AIAA JOURNAL, 1987, 25 (12) : 1631 - 1633
  • [28] Cone Algorithm of Spinning Vehicles under Dynamic Coning Environment
    Zhang, Shuang-biao
    Li, Xing-cheng
    Su, Zhong
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2015, 2015
  • [29] Three descriptions of coning motion and its influence
    Yu, Yang
    Zhang, Hongyue
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2008, 34 (08): : 956 - 960
  • [30] STRAPDOWN GYRO CONTRIBUTION TO CONING MOTION ERRORS
    COFFEE, JR
    SAGGIO, F
    IEEE INTERNATIONAL CONFERENCE ON SYSTEMS ENGINEERING ///, 1989, : 55 - 58