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
  • [21] Robust Velocity Control of a Fixed Canard Decoupled Dual-Spin Projectile
    Nayak, Sandeep Mohan
    Singh, Jitendra
    Kothari, Mangal
    Sahoo, Soumya Ranjan
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2025, 61 (01) : 1079 - 1089
  • [22] A guidance and control design with reduced information for a dual-spin stabilized projectile
    Yu Wang
    Jiyan Yu
    Xiaoming Wang
    Jia Fangxiu
    Defence Technology, 2024, 33 (03) : 494 - 505
  • [23] Multidisciplinary design optimization of a dual-spin guided vehicle
    Karimi, Jalal
    Rajabi, Mohammad Reza
    Sadati, Seyed Hossein
    Hosseini, Seyed Mahid
    DEFENCE TECHNOLOGY, 2024, 37 : 133 - 148
  • [24] Multidisciplinary design optimization of a dual-spin guided vehicle
    Jalal Karimi
    Mohammad Reza Rajabi
    Seyed Hossein Sadati
    Seyed Mahid Hosseini
    DefenceTechnology, 2024, 37 (07) : 133 - 148
  • [25] Influence of yawing force frequency on angular motion and ballistic characteristics of a dual-spin projectile附视频
    Yu WANG
    Jie CHENG
    Ji-yan YU
    Xiao-ming WANG
    Defence Technology, 2016, (02) : 124 - 128
  • [26] Gain-Scheduled Autopilot Design with Anti-Windup Compensator for a Dual-Spin Canard-Guided Projectile
    Thai, Sovanna
    Theodoulis, Spilios
    Roos, Clement
    Biannic, Jean-Marc
    Proff, Michael
    2020 IEEE CONFERENCE ON CONTROL TECHNOLOGY AND APPLICATIONS (CCTA), 2020, : 156 - 161
  • [27] Modeling and Analysis of Rudder Nonlinear Control Force for Dual-spin Projectile with Canards
    Zhao, Xinxin
    Shi, Jinguang
    Wang, Zhongyuan
    Zhang, Ning
    Binggong Xuebao/Acta Armamentarii, 2024, 45 (08): : 2607 - 2616
  • [28] Linearized motion of a fin-stabilized projectile subjected to a lateral impulse
    Guidos, BJ
    Cooper, GR
    JOURNAL OF SPACECRAFT AND ROCKETS, 2002, 39 (03) : 384 - 391
  • [29] Autopilot Design for Dual-Spin Projectile based on PI and Feedback Linearization Control
    Lee, HanJin
    Lee, Chang-Hun
    Jun, Byung-Eul
    2014 IEEE CONFERENCE ON CONTROL APPLICATIONS (CCA), 2014, : 2084 - 2088
  • [30] Roll Control of Course Correction Fuze for Dual-Spin Projectile with Fixed-Canards
    Zhang X.
    Yao X.-X.
    Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology, 2020, 40 (04): : 386 - 395