Title :
Conceptual design of a type fuze of oscillating nose cone for two-dimension trajectory correction
Author :
Jing, Han ; Hua, Wang
Author_Institution :
Sch. of Astronaut., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
Abstract :
A design scheme for two-dimension trajectory correction fuze, actuating by oscillating its nose cone was proposed. Based on the design criterions of compatibility, safety, reliability and economics the structure of oscillating nose cone integrating with the original fuze system was built. The dynamic simulations for some low rolling rocket were performed by using the six degree-of-freedom control ballistic equations. The results show that the principle of oscillating nose cone for fuze is able to realize the function of two-dimension trajectory correction.
Keywords :
ballistics; military systems; position control; reliability; safety; weapons; compatibility design criterion; conceptual design; degree of freedom control ballistic equation; oscillating nose cone; reliability; rolling rocket; safety; two dimension trajectory correction fuze; Equations; Force; Mathematical model; Nose; Projectiles; Rockets; Trajectory; actuating mechanism; fuze; oscillation nose cone; two-dimension trajectory correction;
Conference_Titel :
Industrial Electronics and Applications (ICIEA), 2011 6th IEEE Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-8754-7
Electronic_ISBN :
pending
DOI :
10.1109/ICIEA.2011.5975809
