Movement Characteristics of a Dual-Spin Guided Projectile Subjected to a Lateral Impulse

被引:5
|
作者
Yang, Zhiwei [1 ]
Wang, Liangming [1 ]
Chen, Jianwei [1 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Power & Engn, Nanjing 210094, Peoples R China
关键词
flight mechanics; dual-spin guided projectile; lateral impulse; angular motion; trajectory correction; analytical solutions; LINEAR-THEORY; DESIGN; GUIDANCE;
D O I
10.3390/aerospace8100309
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, a new dual-spin guided projectile that is equipped with ten lateral impulse jets is proposed for trajectory correction. To guide the overall design of the projectile and the control system, a linear motion model of the projectile that was subjected to a lateral impulse was obtained based on a full nonlinear seven-degree-of-freedom (7-DOF) dynamic model. The trajectory correction process of a lateral impulse was divided into two stages. To explain the principle of lateral impulse trajectory correction, the analytical solutions of the linear model of these two stages were obtained. Analytical and numerical solutions were compared to verify the accuracy of the linear model. It is concluded that the analytical and numerical solutions are in good agreement.</p>
引用
收藏
页数:17
相关论文
共 50 条
  • [41] Nonlinear Angular Motionand Bifurcation Characteristics of Canard Dual-Spin Projectiles
    Zhao X.
    Shi J.
    Wang Z.
    Zhang N.
    Binggong Xuebao/Acta Armamentarii, 2023, 44 (10): : 3067 - 3078
  • [42] Analysis of dynamic characteristics of fixed-wing dual-spin projectiles
    Xu, Nuo
    Yu, Jian-Qiao
    Wang, Ya-Fei
    Wang, Lin-Lin
    Binggong Xuebao/Acta Armamentarii, 2015, 36 (04): : 602 - 609
  • [43] Nonlinear dynamics characteristics of a magnetically actuated dual-spin capsule robot
    Huiyuan Yang
    Zhigang Zhou
    Yugong Dang
    Xiaoyi Wang
    Genggeng Li
    Zhidong Xu
    Nonlinear Dynamics, 2023, 111 : 20771 - 20792
  • [44] Analysis of angular motion of dual-spin projectile with fixed-canards under period average control
    Zhang X.
    Yao X.
    Yang Z.
    Guo Z.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2019, 40 (04):
  • [45] Flight Stability of Canard-Guided Dual-Spin Projectiles with Angular Rate Loops
    Zheng, Qiushi
    Zhou, Zhiming
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2020, 2020 (2020)
  • [46] Robust Adaptive Control of Roll Position of Fixed Rudder for Dual-spin Projectile with Improved LuGre Friction Model
    Yin T.
    Jia F.
    Yu J.
    Wang X.
    Binggong Xuebao/Acta Armamentarii, 2019, 40 (12): : 2425 - 2432
  • [47] MODELING AND SIMULATION OF BALLISTIC CHARACTERISTICS FOR DUAL-SPIN STABILIZED PROJECTILES EQUIPPED WITH CANARDS
    Chang, Sijiang
    Qian, Linfang
    Wang, Zhongyuan
    28TH INTERNATIONAL SYMPOSIUM ON BALLISTICS, VOLS 1 AND 2, 2014, : 557 - 567
  • [48] Unsteady aerodynamic modeling and flight trajectory simulation of dual-spin projectile based on DNN and transfer-learning
    Ji, Wen
    Gong, Chunlin
    Jia, Xuyi
    Li, Chunna
    Wang, Gang
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 155
  • [49] Attitude stability of a dual-spin spacecraft on a stationary orbit around an asteroid subjected to gravity gradient torque
    Zhang, Ming-Jiang
    Zhao, Chang-Yin
    ASTROPHYSICS AND SPACE SCIENCE, 2015, 355 (02) : 203 - 212
  • [50] Lateral-Directional Aerodynamics of a Canard Guided Spin Stabilized Projectile at Supersonic Velocity
    Ji Xiuling
    Wang Haipeng
    Zeng Shiming
    Jia Chenyang
    MECHANICAL AND AEROSPACE ENGINEERING, PTS 1-7, 2012, 110-116 : 4343 - +