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《Tactical Missile Technology》 2014-01
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Design of Horizontal Flight Trajectory for Supersonic Rocket Target Based on Controlled Scheme

Zhang Yan;Shan Shizhuo;Unit 92941 Element 93;  
Considering the more defects exist in the no controlled scheme for achieving horizontal flight,a design idea about achieving the horizontal flight by assembling canard control vane and simple control system on the prototype rocket projectile is put forward,and the system concept is described. In the end, according to the aerodynamic characteristic data and missile structure data,the flight trajectory under the different condition are analyzed by using simulation calculations,and combining with the results,the concept of supplying target are analyzed. The result of trajectory simulation indicates that a more straight smooth flight trajectory could be gained by choosing the different launch angle and the control program of rudder deflection angle.
【CateGory Index】: TJ415
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