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

fYear

2011

fDate

21-23 June 2011

Firstpage

1412

Lastpage

1414

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;

fLanguage

English

Publisher

ieee

Conference_Titel

Industrial Electronics and Applications (ICIEA), 2011 6th IEEE Conference on

Conference_Location

Beijing

ISSN

pending

Print_ISBN

978-1-4244-8754-7

Electronic_ISBN

pending

Type

conf

DOI

10.1109/ICIEA.2011.5975809

Filename

5975809