Relative Circular Navigation Guidance for the Impact Angle Control Problem

被引：19
|
作者：
Yoon, Myung-Gon [1 ]
机构：
[1] Kangnung Natl Univ, Dept Precis Mech Engn, Kangnung 201702, Kangwon, South Korea
来源：
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2008年 / 44卷 / 04期
关键词：
D O I：
10.1109/TAES.2008.4667721
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A new homing navigation guidance law is presented for a pursuer to intercept a moving target with a prescribed impact angle: the impact angle control problem. The proposed guidance law can solve the Impact angle control problem for virtually every initial geometry of pursuer and target on a plane and any desired impact attitude angle. The impact angle error of the proposed law is presented in a closed form. In addition it is shown that the acceleration command is finite even at impact time. A comparative study with existing techniques is performed both analytically and numerically to investigate the performance and properties of the new law.
引用
收藏
页码：1449 / 1463
页数：15
相关论文
共 50 条
  • [41] Terrestrial Testing of Multi-Agent, Relative Guidance, Navigation, and Control Algorithms
    Mercier, Mark
    Phillips, Sean
    Shubert, Matt
    Dong, Wenjie
    2020 IEEE/ION POSITION, LOCATION AND NAVIGATION SYMPOSIUM (PLANS), 2020, : 1488 - 1497
  • [42] Guidance and Control System Design for Impact Angle Control of Guided Bombs
    Kim, Yongho
    Kim, Jongju
    Park, Minsu
    INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS (ICCAS 2010), 2010, : 2138 - 2143
  • [43] Optimal control based guidance law to control both impact time and impact angle
    Chen, Xiaotian
    Wang, Jinzhi
    AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 84 : 454 - 463
  • [44] Polynomial guidance law for impact angle control with a seeker look angle limit
    Zhou, Zhiming
    Yao, Xiaoxian
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2020, 234 (03) : 857 - 870
  • [45] Analytical solution of pure proportional navigation guidance law and three-dimensional guidance with impact angle constraint
    Liao X.
    Li K.
    Liu Y.
    Chen L.
    Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2021, 53 (12): : 42 - 50
  • [46] Relative navigation and guidance technologies for rendezvous and docking
    An Kai
    Tang Zhaoting
    2013 THIRD INTERNATIONAL CONFERENCE ON INSTRUMENTATION & MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC), 2013, : 1228 - 1232
  • [47] Minimum-Data-Driven Guidance for Impact Angle Control
    Liu, Chang
    Wang, Jiang
    Li, Hongyan
    Liu, Weipeng
    AEROSPACE, 2024, 11 (05)
  • [48] An Optimal Geometrical Guidance Law for Impact Time and Angle Control
    Hou, Libing
    Luo, Haowen
    Shi, Heng
    Shin, Hyo-Sang
    He, Shaoming
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2023, 59 (06) : 9821 - 9830
  • [49] Direct impact angle control guidance for passive homing missiles
    Cho, Dongsoo
    Kim, Seung-Hwan
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2020, 234 (15) : 2139 - 2152
  • [50] Integrated Guidance and Control with Input Saturation and Impact Angle Constraint
    Fu, Zhenhua
    Zhang, Kuanqiao
    Gan, Qintao
    Yang, Suochang
    DISCRETE DYNAMICS IN NATURE AND SOCIETY, 2020, 2020
12345