[1] [1] GENG D P , WANG ZH P.Design and implementation of hardware-in-the-loop simulation system for missile control and guidance system［J］.Flight Dynamics,2008,26(5):75-77.(in Chinese)

[2] [2] SUN R SH, LIANG ZH.Analysis of a hardware-in-the-loop simulation of GB’s guidance and control system with orthogonal test［J］.Acta Armamentarii,2008,29(7):883-886.(in Chinese)

[3] [3] LI X.Realize of a hardware-in-the-loop simulation of guided bomb ［J］.Journal of System Simulation,2009,5(5):49-52.(in Chinese)

[4] [4] HAN SH P， HUANG K D.Research of time advancing mechanism for DEVS/HLA distributed simulation［J］.Journal of System Simulation,2008,20(7):1744-1748.(in Chinese)

[5] [5] ZHANG J N, HUANG K D.Precision analysis and simulation of cruise missile middle guidance ［J］.Aero Weaponry.2007(1):25-27.(in Chinese)

[6] [6] ZHANG G,LIU X T,LIU L.Research on imaging guidance semi physical simulation system design［J］.Modern Defense Technology,2006,34(6):111-114.(in Chinese)

[7] [7] FANG Y H.Simulation of Antiaircraft Missile ［M］.Beijing：Aeronautics and Astronautics Press of China , 1995.(in Chinese)

[8] [8] MENG X Y.Principle of Missile Guidance and Control System［M］.Beijing： Beijing Institute of Technology Press,2003.

[9] [9] PETER H Z.Modeling and Simulation of Aerospace Vehicle Dynamics［M］.Florida： America Institute of Aeronautics and Astronautics, 2000.(in Chinese)

[10] [10] ZHANG Y J.Design of Tactical Missile Flight Mechanics［M］.Beijing：Aeronautics and Astronautics Press of China, 1996.(in Chinese)