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A study of adaptive angle TF(Terrain Following)algorithm and the flight control system of missile have been carried out. From digital simulations, it is shown that the algorithm of adaptive angle command is closely related to the design of flight control system, and the missile is able to fly safely by using Digital Elevation Model(DEM)without Terrain Following Radar.
1 朱晨辉.地形跟踪仿真系统研究[硕士论文].南京航空航天大学,1992
2 郑衍杲.超低空突防中的地形跟随/回避技术.航空学报,1985,8(6)
3 张明廉.飞行控制系统.北京:航空工业出版社,1994
4 钱杏芳,等.导弹飞行力学,北京工业学院出版社,1987
Basic Information:
DOI：10.16358/j.issn.1009-1300.1998.02.010
China Classification Code:TJ765
Citation Information:
[1]Wang Changqing,Li Jingyuan The Third Research Academy of CASC.AN APPROACH TO THE DESIGN OF TERRAIN FOLLOWING CONTROL SYSTEMS[J].Tactical Missile Technology,1998(02):35-39+55.DOI:10.16358/j.issn.1009-1300.1998.02.010.
1998-06-15
1998-06-15