[1] [1] LIU X T.Precision Guidance& Control and Simulation Technology [M].Beijing:National Defense Industry Press,2006.(in Chinese)

[2] [2] QU Y L.Ballistae Meteorology [M].Beijing:China Meteorology Press,1987.(in Chinese)

[3] [3] TANG SH J,YUAN Z H.Design of flight mechanics software system of tactical missiles [J].Flight Dynamics,1997,15(2):81-85.(in Chinese)

[4] [4] ZHANG L,JIANG H ZH,QI F G,et al..Flight simulation based on MATLAB [J].Computer Simulation,2006,23(6):57-59.(in Chinese)

[5] [5] ZHANG Y,LIU B,YIN SH L.Strapdown optical seeker:stabilization tracking principle and system simulation [J].Opt.Precision Eng.,2008,16(10):1943-1945.(in Chinese)

[6] [6] LEWIS B L,STEVENS F L.Aircraft Control and Simulation [M].New York:John Wiley& Sons,1992.

[7] [7] ZHANG R H,JIA H G,CHEN T, et al..Attitude solution for strapdown inertial navigation system based on quaternion algorithm [J] .Opt.Precision Eng.,2008,16(10):1964-1965.(in Chinese)

[8] [8] ZHANG Y J.Design of Flight Dynamic [M].Beijing:China Astronautic Publishing House,1995.(in Chinese)

[9] [9] COOK M V.Flight Dynamics Principles [M] .UK:Butterworth-Heinemann,1997.

[10] [10] GJB365.1-87.Standard atmosphere of the northern hemisphere[S].(in Chinese)

[11] [11] SUTTON G P,BIBLARZ O.Rocket Propulsion Elements [M] .New York:John Wiley& Sons,2001.

[12] [12] ZIPFEL P H.Modeling and Simulation of Aerospace Vehicle Dynamic [M] .Virginia:American Institute of Aeronautics and Astronautics,2007.

[13] [13] CHEN Y X,KANG R,SUN Y F.Study on reliability simulation for flight control system under the influence of wind [J] .Journal of System Simulation,2005,12(2):276-278.(in Chinese)

[14] [14] QIAN X F,LIN R X,ZHAO Y N.Flight Dynamic of Missile [M] .Beijing:Beijing Institute of Technology Press,2000.(in Chinese)

[15] [15] LI M,JI Y,JIA H G,et al..Hardware-in-closed-loop simulation for aircraft based on rapid simulation prototype [J].Opt.Precision Eng.,2008,16(10):1950-1951.(in Chinese)