Relaxed Stable Stability Technology for an Air-to-air Missile

被引:0
|
作者
GUO Zheng-yu
机构
关键词
missile; active control technology; relaxed stable stability; new future missiles;
D O I
10.13434/j.cnki.1007-4546.2012.02.008
中图分类号
TJ762.23 [];
学科分类号
摘要
Relaxed Stable Stability(RSS) in an important part of the active control technology.It is a new way to raise the flying speed,distance and maneuverability of missile.Depth study of RSS technology plays an important role for the new concept missile design.This paper describes the detailed definition of RSS and its advantages,presents the research status and prospects for its application in the design of new missiles.
引用
收藏
页码:112 / 116
页数:5
相关论文
共 50 条
  • [21] DEVELOPMENT OF THE AERODYNAMIC CONFIGURATION FOR AN ADVANCED AIR-TO-AIR MISSILE
    BROOKS, WB
    PRILLIMAN, FW
    ASTRONAUTICS & AERONAUTICS, 1979, 17 (7-8): : B42 - B42
  • [22] 3-DIMENSIONAL AIR-TO-AIR MISSILE TRAJECTORY SHAPING
    KUMAR, RR
    SEYWALD, H
    CLIFF, EM
    KELLEY, HJ
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1995, 18 (03) : 449 - 456
  • [23] Flush air data sensing system design for air breathing air-to-air missile
    Chen G.
    Liu W.
    Dou X.
    Zhou W.
    Dou G.
    Chen, Guangqiang (guangqiangchen@sina.com), 1600, Chinese Academy of Sciences (46): : 1193 - 1206
  • [24] Raytheon and MBDA battle for air-to-air missile market share
    不详
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2007, 79 (03): : 296 - 296
  • [25] EIGENSTRUCTURE ASSIGNMENT FOR THE EXTENDED MEDIUM RANGE AIR-TO-AIR MISSILE
    SOBEL, K
    CLOUTIER, JR
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (02) : 529 - 531
  • [26] Separation Dynamics of Air-to-Air Missile and Validation with Flight Data
    Anandhanarayanan, K.
    Raj, Ankit
    Shah, Vaibhav
    Krishnamurthy, R.
    Chakraborty, Debasis
    DEFENCE SCIENCE JOURNAL, 2018, 68 (01) : 5 - 11
  • [27] Effects of datalink target data on air-to-air missile performance
    Ostrom, John
    Sailaranta, Timo
    Virtanen, Kai
    JOURNAL OF DEFENSE MODELING AND SIMULATION-APPLICATIONS METHODOLOGY TECHNOLOGY-JDMS, 2024, 21 (03): : 323 - 340
  • [28] A Near Optimal Midcourse Guidance Law for Air-to-Air Missile
    Qiao Qingqing
    Chen Wanchun
    INDUSTRIAL INSTRUMENTATION AND CONTROL SYSTEMS II, PTS 1-3, 2013, 336-338 : 833 - 838
  • [29] Coefficient diagram robust control design for air-to-air missile
    Zhao, Jinlei
    Cao, Junyi
    Ma, Chengbin
    Zhou, Shengxi
    Cao, Binggang
    Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2013, 47 (11): : 70 - 75
  • [30] AIR-TO-AIR MISSILE AIRFRAME CAPTIVE FLIGHT VIBROACOUSTIC ENVIRONMENT
    POYNOR, SP
    JOURNAL OF THE IES, 1990, 33 (04): : 44 - 52