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Articles:2012,Vol:17,Issue(2):112-116 |
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Citation: |
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GUO Zheng-yu, LIANG Xiao-geng. Relaxed Stable Stability Technology for an Air-to-air Missile[J]. International Journal of Plant Engineering and Management, 2012, 17(2): 112-116 |
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| Relaxed Stable Stability Technology for an Air-to-air Missile |
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| GUO Zheng-yu, LIANG Xiao-geng |
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| Luoyang Opto-Electro Technology Development Center,Luoyang 471000,P. R. China |
| Abstract: |
| 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. |
| Key words:
missile
active control technology
relaxed stable stability
new future missiles
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| Received: 2012-05-20
Revised:
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| DOI: |
| Corresponding author:
Email：inter5678@si-na.com |
| Author description:
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References: |
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[1] Xing X L，Liu static stability toDJ，lpplacataouoverall design of air-to-air missile. Flight Dynamics，20 (3)，2002(In Chinese)
[2] Zhou H Z，Li Z Y，Analysis of Longitudinal stability problem of relaxed static stability air-craft. Winged Missiles Journal (2)，1998 (In Chinese)
[3] Yang Y B，Guo C W，Relaxed static stability on the application of the Loug-range cruise mis-siles. China Flight Dynamics Conference，1995 (In Chinese)
[4] Liu D J，The application of active control tech-nology to air to air missiles. Tactical Missile Technology，(5)，2001 (In Chinese)
[5] Li S X，Zhang Y A，Yin X Q，Control system design of static unstable missile using three Loop acceleration based on simulink parameters optimizing. Journal of Naval aeronautical En-gineering Institute，25 (2)，2010(In Chi-nese)
[6] Alhright A E，Dixon C J，Hegedus M C，Modi-fication and validation of conceptual design aero-dynamic prediction method. HASC95 with VTX-CHN，NASA CR-712，March 1996
[7] Li B L} Relaxed stable stability missile control Law design. Flight Dynamics，(2)，1985 (In Chinese)
[8] Ruhen E. Perez，Hugh H T，Liu，Kamran Beh-dinan，Relaxed static stability aircraft design via Longitudinal control-configured MDO methodolo-gy. CASI Conference on Aerospace Technology and Innovation, Aircraft Design&Development Symposium Toronto，ON，April 26-27，2005 (In Chinese)
[9] Blight J D，Gangsaas D，Richardson T M，Control Law synthesisfor an airplane with re-laxed static stability. Guidance，Control and Dynamics，9 (5 )，Sept-Oct, 1986
[10] Guo F T，Guan C Q，Research on the influence of relaxed static stability on missile capability. Tactical Missile Technology，(6 )，2007(In Chinese)
[l1] Tang S J，Dynamic varied extension of the mis-site static-stability. Journal of Beijing Institute of Technology(19):678-681，1999 (In Chi-nese)
[12] Yin B S，Huang Z A，Design and analysis offlight control system for statically unstableback-to-turn missile. Journal of Nanjing Uni-versity of Aeronaustics&Astronautics，Nov，25:22-25，1993 (In Chinese)
[13] Wang G L，Chai X，Wu Z，Research on im-proving flying wing take off performance withLongitudinal static instability. Flight Dynam-ics，27:10-14，2009 (In Chinese)
[14] Wise Kevin A，Bory David J, Agile missile dy-namic and control. AIAA Paper 96-3912
[15] Sweetman Bill，Russian short and visual-rangeair-to-air missiles. Air&Space，9 (4)，1994
[16] Anderson B 0 0，Topical problems of adaptivecontrol. in Proc. European Control Confer-ence，Kos. Greece. 4997-4998, 2007 |
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