• Optics and Precision Engineering
  • Vol. 24, Issue 9, 2262 (2016)
HAN Xue-feng*, LIU Xiao-dong, MA Wu-yuan, MA Qing, and YUAN Dong-ming
Author Affiliations
  • [in Chinese]
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    DOI: 10.3788/ope.20162409.2262 Cite this Article
    HAN Xue-feng, LIU Xiao-dong, MA Wu-yuan, MA Qing, YUAN Dong-ming. Optimization and experiments of deployment performance for folding wing mechanism of an aircraft[J]. Optics and Precision Engineering, 2016, 24(9): 2262 Copy Citation Text show less
    References

    [1] ZHOU Y, ZHOU X B, WANG Z Y.“Gem” laser guided bombs and wind and rain forty years [J].Weapon Expo., 2006(2): 5-9.(in Chinese)

    [2] DING H.Finite Element Analysis and Ex Perimental Study for Afolding Wing of Aircraftmissiles [D].Harbin: Harbin Engineering University, 2010.(in Chinese)

    [3] ZHANG M Y, YANG H B, ZHANG J B. Servo system of harmonic drive electromechanical actuator using improved ADRC [J]. Opt. Precision Eng., 2014, 22(1): 99-106.(in Chinese)

    [4] XIAO Q J, JIA H G, ZHANG J B, et al.. Identification and compensation of nonlinearity for electromechanical actuator servo sysem [J].Opt. Precision Eng., 2013, 21(8): 2038-2046.(in Chinese)

    [5] ROBERT K. Wing mechanism analysis [J]. Computers and Structures, 1999, 72(8): 253-265.

    [6] YUDI H, HOON C P, NAM S G. Byun Design and demonstration of a small expandable morphing wing [J]. Proc.of SPIE, 2005, 57(14): 224-231.

    [7] METOM S.Piezoelectrically actuated four-bar mechanism with two flexible links for micromechanical flying insect thorax [J].IEEE/ASME Transactions on Mechatronics, 2003, 104(1): 299-305.

    [8] MA C X, YU X D, WANG T.Missile folding wing exercise testing [J].Journal of Projectiles, Rockets, MissilesandGuidance, 1993(2): 63-65.(in Chinese)

    [9] LI X H, LI H N, WU J Q.Calculation and experimental study on the folding wing of rocket projectile [J]. Spacecraft Environment Engineering, 2009, 26: 82-86.(in Chinese)

    [10] CUI E W, YU C G, LI M, et al..The simulation analysis of the wing of a missile folding wing [J].Ordnance Industry Automation, 2013, 32(12): 12-15.(in Chinese)

    [11] WU J Q, SUN H W, ZHANG X.The researchon unfolding testand dynamic model of folding-wing [J]. Journal of Projectiles, Rockets, MissilesandGuidance, 2012, 32(3): 164-167.(in Chinese)

    [12] ZHAO J F, LIU L. Dynamic simulation and optimization design of folding wing deployment [J]. Journal of Projectiles, Rockets, MissilesandGuidance, 2011, 31(5): 141-146.(in Chinese)

    [13] CLOUGH R W, PENZIEN J, WANG G Y(Translation).Structural Dynamics [M]. Beijing: Higher Education Press, 2006.(in Chinese)

    [14] JIN G, XIE X G, GU S.Dynamic simulation and application of deploy able mechanism of satellite solar panels [J].Opt. Precision Eng., 2014, 22(3): 745-751.(in Chinese)

    [15] ZHENG L M, DENG CH P, YANG ZH H.Dynamic simulation and application of deployable mechanism of satellite solar panels [J]. Opt. Precision Eng., 2009, 17(12): 3047-3054.(in Chinese)

    [16] HEI M, LU Y F, ZHANG ZH Y.Design of fast steering mirror based on dynamic model [J].Opt. Precision Eng., 2013, 21(1): 53-61.(in Chinese)

    [17] HUANG R Z, WAN J Q, MA H W.Optimization of synthetic culture condition ofcellulose producing strains using orthogonal experimental design [J].China Environmental Science, 2012, 32(1): 130-135.(in Chinese)

    [18] LIU G H, LIU W, LIU ZH. Using the four factor three level orthogonal regression analysis method to study the prediction of drilling string [J].Journal of Oil and Gas Technology, 2010, 32(3): 108-112.(in Chinese)

    [19] ZHENG X Y, JIA ZH Y, REN X T.Analysis on effect of discharge parameters on cylindricity of small holes by orthogonal experiments [J].Opt. Precision Eng., 2010, 18(2): 426-433.(in Chinese)

    HAN Xue-feng, LIU Xiao-dong, MA Wu-yuan, MA Qing, YUAN Dong-ming. Optimization and experiments of deployment performance for folding wing mechanism of an aircraft[J]. Optics and Precision Engineering, 2016, 24(9): 2262
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