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
收藏
页码:2369 / 2378
页数:10
相关论文
共 50 条
  • [31] Optimal design of a passive coning attenuator for spinning spacecraft under thrust
    Halsmer, DM
    Fetter, AR
    SPACEFLIGHT MECHANICS 1998, VOL 99, PTS 1 AND 2, 1998, 99 : 601 - 610
  • [32] GAS-DYNAMIC FLOW IN A SPINNING, CONING SOLID ROCKET MOTOR
    MISTEREK, DL
    MURDOCK, JW
    KOSHIGOE, S
    JOURNAL OF PROPULSION AND POWER, 1993, 9 (01) : 35 - 42
  • [33] Constrained optimization of passive coning attenuators for spinning spacecraft under thrust
    Lang, A
    Halsmer, D
    SPACEFLIGHT MECHANICS 2001, VOL 108, PTS 1 AND 2, 2001, 108 : 155 - 162
  • [34] PRESSURE MEASUREMENTS OF A ROTATING LIQUID FOR IMPULSIVE CONING MOTION
    DAMICO, WP
    BEIMS, WG
    ROGERS, TH
    JOURNAL OF SPACECRAFT AND ROCKETS, 1983, 20 (02) : 99 - 100
  • [35] Coning motion stability of wrap around fin rockets
    XueRui Mao
    ShuXing Yang
    Yong Xu
    Science in China Series E: Technological Sciences, 2007, 50 : 343 - 350
  • [36] Coning motion stability of wrap around fin rockets
    MAO XueRui
    Science China Technological Sciences, 2007, (03) : 343 - 350
  • [37] A Coning Compensation Algorithm for SINS in High Dynamic Motion
    Li, Zongtao
    Wu, Tiejun
    Ma, Longhua
    CONTROL ENGINEERING AND APPLIED INFORMATICS, 2011, 13 (03): : 32 - 40
  • [38] Coning motion stability of wrap around fin rockets
    Mao XueRui
    Yang ShuXing
    Xu Yong
    SCIENCE IN CHINA SERIES E-TECHNOLOGICAL SCIENCES, 2007, 50 (03): : 343 - 350
  • [39] Numerical study of viscous flows inside partially filled spinning and coning cylinders
    Selmi, M
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 1996, 118 (02): : 335 - 340
  • [40] Numerical study on the aerodynamic coupling effects of spinning and coning motions for a finned vehicle
    Lu, Tianyu
    Wu, Xiaosheng
    Lei, Juanmian
    Yin, Jintao
    AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 77 : 399 - 408