Research on the Attitude Control Law of Hypersonic Flight Vehicle

被引：0
|
作者：
Zhou, Hongcheng [1 ,2 ]
Wang, Daobo [2 ]
Yang, Juan [1 ]
机构：
[1] JinLing Inst Technol, Inst Informat, Nanjing 211169, Jiangsu, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Jiangsu, Peoples R China
来源：
IAEDS15: INTERNATIONAL CONFERENCE IN APPLIED ENGINEERING AND MANAGEMENT | 2015年 / 46卷
关键词：
SMALL-SCALE HELICOPTER; TRACKING CONTROL; UAV HELICOPTER;
D O I：
10.3303/CET1546027
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
Hypersonic flight vehicle has strong-nonlinearity, quick time-variability, strong-coupling features. In order to realize its flight effective control, the airflow attitude angle needs to be controlled precisely. Based on the accurate tracking of the airflow attitude angle command, the predetermined flight path can be realized to accomplish flight tasks. Use dynamic surface (DSC) to design the airflow angle attitude control law, which proves the stability and the time-delay compensation effect. The simulation results show that this method has good tracking control and fast convergence.
引用
收藏
页码：157 / 162
页数：6
相关论文
共 50 条
  • [1] Attitude optimization control of hypersonic flight vehicle considering partially unknown control direction
    Guo, Jianguo
    Wang, Jiaqi
    Guo, Zongyi
    Su, Yalu
    [J]. TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2023, 45 (07) : 1337 - 1350
  • [2] Research Progress and Prospect of the Hypersonic Flight Vehicle Control Technology
    Zhang, Yuan
    Huang, Xu
    Lu, Kunfeng
    Bai, Wenyan
    Huang, Wanwei
    [J]. Yuhang Xuebao/Journal of Astronautics, 2022, 43 (07): : 866 - 879
  • [3] Discrete reconfigurable back-stepping attitude control of reentry hypersonic flight vehicle
    Ren, Zijun
    Fu, Wenxing
    Yan, Jie
    Xu, Bin
    [J]. ADVANCES IN MECHANICAL ENGINEERING, 2017, 9 (04) : 1 - 10
  • [4] Stochastic precision analysis of hypersonic flight vehicle attitude control system in the presence of uncertainties
    Jiang, Ruimin
    Zhou, Jun
    Guo, Jianguo
    [J]. SYSTEMS SCIENCE & CONTROL ENGINEERING, 2020, 8 (01): : 277 - 287
  • [5] Attitude Control of Unmanned Hypersonic Test Vehicle
    Wang, Xin
    Feng, Dongzhu
    Lin, Yi
    [J]. 2008 2ND INTERNATIONAL SYMPOSIUM ON SYSTEMS AND CONTROL IN AEROSPACE AND ASTRONAUTICS, VOLS 1 AND 2, 2008, : 1113 - +
  • [6] The Nonlinear Adaptive Attitude Control for Hypersonic Vehicle
    [J]. Hu, Jun (hujunbice@126.com), 1600, China Spaceflight Society (38):
  • [7] Switching Control Design for A Hypersonic Flight Vehicle
    Tan, Shuping
    Li, Zhibin
    [J]. 2010 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-5, 2010, : 3568 - 3573
  • [8] Fuzzy adaptive non-affine attitude tracking control for a generic hypersonic flight vehicle
    Wang, Yuhui
    Chen, Mou
    Wu, Qingxian
    Zhang, Jun
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 80 : 56 - 66
  • [9] Dynamic Characteristic and Control of a Hypersonic Flight Vehicle
    Qin, Dongsheng
    Zhu, Qiangjun
    Wang, Chenxi
    [J]. PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON COMPUTER, NETWORKS AND COMMUNICATION ENGINEERING (ICCNCE 2013), 2013, 30 : 29 - 33
  • [10] Self-Healing Control for Attitude System of Hypersonic Flight Vehicle With Body Flap Faults
    Wang, Ang
    Chen, Fuyang
    Gong, Huajun
    [J]. IEEE ACCESS, 2018, 6 : 19121 - 19130
12345