Effect of seeker disturbance rejection rate parasitic loop on performance of optimal guidance law

被引：1
|
作者：
机构：
[1] Li, Fugui
[2] Xia, Qunli
[3] Qi, Zaikang
来源：
Xia, Q. (1010@bit.edu.cn) | 1600年 / Chinese Society of Astronautics卷 / 34期
关键词：
D O I：
10.7527/S1000-6893.2013.0359
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [31] The effect of seeker and autopilot dynamics on the performance of proportional navigation guidance
    Qi, ZK
    Liu, D
    SINO-RUSSIA INTERNATIONAL ACADEMIC CONFERENCE, PROCEEDING, 2000, : 16 - 19
  • [32] On the Active Disturbance Rejection Control Based Guidance Law Design with Angle Constraint
    Yang Xiaoyan
    Li Donghai
    Lao Dazhong
    2014 33RD CHINESE CONTROL CONFERENCE (CCC), 2014, : 770 - 775
  • [33] Disturbance rejection performance analyses of closed loop control systems by reference to disturbance ratio
    Alagoz, Bans Baykant
    Deniz, Furkan Nur
    Keles, Cemal
    Tan, Nusret
    ISA TRANSACTIONS, 2015, 55 : 63 - 71
  • [34] OPTIMAL PERFORMANCE IN TRACKING STOCHASTIC SIGNAL UNDER DISTURBANCE REJECTION
    Zhan, Xi-Sheng
    Guan, Zhi-Hong
    Liao, Rui-Quan
    Yuan, Fu-Shun
    ASIAN JOURNAL OF CONTROL, 2012, 14 (06) : 1608 - 1616
  • [35] OPTIMAL DISTURBANCE REJECTION AND PERFORMANCE ROBUSTNESS IN LINEAR-SYSTEMS
    SUBRAHMANYAM, MB
    JOURNAL OF MATHEMATICAL ANALYSIS AND APPLICATIONS, 1992, 164 (01) : 130 - 150
  • [36] Design of cascade active disturbance rejection guidance law for miniature strapdown guided munition
    Chen, Shiwei
    Fan, Junfang
    Wang, Haisen
    Mu, Qingdong
    PROCEEDINGS OF THE 33RD CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2021), 2021, : 4765 - 4770
  • [37] Design and Optimization of Carrier Landing Guidance Law Using Active Disturbance Rejection Controller
    Li Ji-xin
    Hou Zhi-qiang
    Zheng Xiao-hong
    2008 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-11, 2008, : 3636 - +
  • [38] Design of closed loop optimal guidance law using neural networks
    Zhou, Rui
    Chinese Journal of Aeronautics, 2002, 15 (02) : 98 - 102
  • [39] Adaptive weighting impact angle optimal guidance law considering seeker's FOV angle constraints
    Li Ran
    Wen Qiuqiu
    Tan Wangchun
    Zhang Yijie
    JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2018, 29 (01) : 142 - 151
  • [40] Optimal guidance law based on inverse optimal problem and performance analysis
    Wang, Jiang, 1600, Journal of Solid Rocket Technology (37):
12345