Robust autopilot design for a beam rider guided missile system

被引：0
|
作者：
Egyptian Armed Forces, Egypt [1 ]
机构：
来源：
Nat Radio Sci Conf NRSC Proc | / C28期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [21] Study on the missile autopilot's design based on robust control theory
    Wu Xiaoyan
    Fan Zongchen
    Zhou Yanyan
    He Guangjun
    ISTM/2007: 7TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1-7, CONFERENCE PROCEEDINGS, 2007, : 5500 - 5503
  • [22] H∞ Robust Gain-Scheduled Autopilot Design for Portable Missile
    Chen Xianxiang
    Song Jianmei
    2011 30TH CHINESE CONTROL CONFERENCE (CCC), 2011, : 2322 - 2326
  • [23] Design of robust autopilot-output integral sliding mode controllers for guided missile systems with parameter perturbations
    Jafarov, EM
    Tasaltin, R
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2001, 73 (01): : 16 - 25
  • [24] Nonlinear Autopilot Design for an Asymmetric Missile Using Robust Backstepping Control
    Mattei, Giovanni
    Monaco, Salvatore
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2014, 37 (05) : 1462 - 1476
  • [25] COMBINED OPTIMAL-CLASSICAL APPROACH TO ROBUST MISSILE AUTOPILOT DESIGN
    NESLINE, FW
    WELLS, BH
    ZARCHAN, P
    JOURNAL OF GUIDANCE AND CONTROL, 1981, 4 (03): : 316 - 322
  • [26] Comparative study of H∞ robust control methods in missile autopilot design
    Le Letty, L
    Jang, SK
    ROBUST CONTROL DESIGN (ROCODN'97): A PROCEEDINGS VOLUME FROM THE IFAC SYMPOSIUM, 1997, : 407 - 412
  • [27] Nonlinear robust missile autopilot design using Successive Galerkin Approximation
    McLain, TW
    Beard, RW
    AIAA GUIDANCE, NAVIGATION, AND CONTROL CONFERENCE, VOLS 1-3: A COLLECTION OF TECHNICAL PAPERS, 1999, : 384 - 391
  • [28] Application on a robust output feedback linearization approach to missile autopilot design
    School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
    不详
    Yuhang Xuebao, 2006, 5 (990-994+1058):
  • [29] Longitudinal robust autopilot design for air-to-air missile using μ synthesis
    College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
    Nanjing Li Gong Daxue Xuebao, 2009, 6 (766-769):
  • [30] Robust Missile Autopilot Design Using Two Time-Scale Separation
    Panchal, Bhavnesh
    Subramanian, K.
    Talole, S. E.
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2018, 54 (03) : 1499 - 1510
12345