Title of article :
Simulation and experimental research on line throwing rocket with flight
Author/Authors :
Gu، نويسنده , , Wen-bin and Lu، نويسنده , , Ming and Liu، نويسنده , , Jian-qing and Dong، نويسنده , , Qin-xing and Wang، نويسنده , , Zhen-xiong and Chen، نويسنده , , Jiang-hai، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2014
Pages :
5
From page :
149
To page :
153
Abstract :
The finite segment method is used to model the line throwing rocket system. A dynamic model of line throwing rocket with flight motion based on Kaneʹs method is presented by the kinematics description of the system and the consideration of the forces acting on the system. The experiment designed according to the parameters of the dynamic model is made. The simulation and experiment results, such as range, velocity and flight time, are compared and analyzed. The simulation results are basically agreed with the test data, which shows that the flight motion of the line throwing rocket can be predicted by the dynamic model. A theoretical model and guide for the further research on the disturbance of rope and the guidance, flight control of line throwing rocket are provided by the dynamic modeling.
Keywords :
Line throwing rocket , flight simulation , Kaneיs method
Journal title :
Defence Technology
Serial Year :
2014
Journal title :
Defence Technology
Record number :
2316905
Link To Document :
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