ISBN: 978-981-09-5471-0 DOI: 10.18178/wcse.2015.04.073
Research on Correction Ability for Simple Guided Artillery Rocket’s Fixed Canard Rudder
Abstract— According to the application requirements of adopting fixed canard rudder technology to
medium and small guidance rocket, a kind of single channel rolling control strategy suitable for
fixed canard rudder was proposed. The working principle of fixed canard rudder was mainly
analyzed. The equations of cycle average control force and moment were deduced. The 6DOF
external ballistic model of the fixed canard rudder was established. The numerical simulation of the
Wing lift was carried out with the Fluent, and the simulation & research of the correction ability
was carried out combining the 6DOF external ballistic equation. According to this, the correcting
ability of the fixed canard rudder was emulated and calculated, the result shows that the correcting
ability is enough by using the rudder, and it’s one of the feasible low cost and the miniaturized
rudder technology.
Index Terms— fixed canard rudder, single glow, rolling control, correction force, ballistic correction
Aitian Yan, Changsheng Zhou, Jinsheng Xu, Jian Li
School of Mechanical Engineering, Nanjing University of Science and Technology, CHINA
Cite: Aitian Yan, Changsheng Zhou, Jinsheng Xu, Jian Li, "Research on Correction Ability for Simple Guided Artillery Rocket’s Fixed Canard Rudder," 2015 The 5th International Workshop on Computer Science and Engineering-Information Processing and Control Engineering (WCSE 2015-IPCE), pp. 443-448, Moscow, Russia, April 15-17, 2015.