TY - GEN
T1 - Research on initial disturbance influenced by adapter combined with guide rail
AU - Liu, Dong
AU - Jiang, Yi
AU - Zhang, Heng
AU - Yang, Zheng Ran
PY - 2014
Y1 - 2014
N2 - Initial disturbance is the chief factor that affects missile launch accuracy and divergence while using orientation devices could reduce it effectively. In this paper, adapter combined with guide rail will be mainly studied. Modeling and simulation for missile systems will be done by virtual prototyping technology, focusing on deflection, pitch angle, and pitch angular velocity and so on to analysis initial disturbance. Results show that by mean of adapter combined with guide rail initial disturbance could be greatly reduced and launch accuracy has been improved.
AB - Initial disturbance is the chief factor that affects missile launch accuracy and divergence while using orientation devices could reduce it effectively. In this paper, adapter combined with guide rail will be mainly studied. Modeling and simulation for missile systems will be done by virtual prototyping technology, focusing on deflection, pitch angle, and pitch angular velocity and so on to analysis initial disturbance. Results show that by mean of adapter combined with guide rail initial disturbance could be greatly reduced and launch accuracy has been improved.
KW - Adapter combined with guide rail
KW - Initial disturbance
UR - http://www.scopus.com/inward/record.url?scp=84892836797&partnerID=8YFLogxK
U2 - 10.4028/www.scientific.net/AMM.488-489.934
DO - 10.4028/www.scientific.net/AMM.488-489.934
M3 - Conference contribution
AN - SCOPUS:84892836797
SN - 9783037859766
T3 - Applied Mechanics and Materials
SP - 934
EP - 937
BT - Materials Science, Civil Engineering and Architecture Science, Mechanical Engineering and Manufacturing Technology
T2 - 2014 International Conference on Advanced Engineering Materials and Architecture Science, ICAEMAS 2014
Y2 - 4 January 2014 through 5 January 2014
ER -