TY - GEN
T1 - Analysis of rudder characteristics of spin missile
AU - Sun, Chunxiang
AU - Mo, Bo
PY - 2011
Y1 - 2011
N2 - Based on hinge moment coefficient of rolling missile which obtained from wind tunnel experiment, the relationships among hinge moment and angle of attack and deflection angle of rudder are derived from fitting and analysis, and then the accelerating torque is calculated by instruction signal of rudder, next the equation to describe load characteristic of rudder is got. According to the equation, the load characteristic curves are drawn with MATLAB software, and the characteristic curves provide a basis for the type selection of motor.
AB - Based on hinge moment coefficient of rolling missile which obtained from wind tunnel experiment, the relationships among hinge moment and angle of attack and deflection angle of rudder are derived from fitting and analysis, and then the accelerating torque is calculated by instruction signal of rudder, next the equation to describe load characteristic of rudder is got. According to the equation, the load characteristic curves are drawn with MATLAB software, and the characteristic curves provide a basis for the type selection of motor.
KW - Spin Missile
KW - hinge momen
KW - load characteristic
KW - load characteristic Curve
UR - http://www.scopus.com/inward/record.url?scp=80955148493&partnerID=8YFLogxK
U2 - 10.1109/ICECENG.2011.6057655
DO - 10.1109/ICECENG.2011.6057655
M3 - Conference contribution
AN - SCOPUS:80955148493
SN - 9781424481637
T3 - 2011 International Conference on Electrical and Control Engineering, ICECE 2011 - Proceedings
SP - 4729
EP - 4732
BT - 2011 International Conference on Electrical and Control Engineering, ICECE 2011 - Proceedings
T2 - 2nd Annual Conference on Electrical and Control Engineering, ICECE 2011
Y2 - 16 September 2011 through 18 September 2011
ER -