The Whole Trajectory Simulation of Cruise Missile Based on Inertial Navigation Error Model

DOI

10.2991/iccsee.2013.65How to use a DOI?

Keywords

Strapdown Inertial Navigation System, Cruise missile, The whole trajectory simulation

Abstract

For the problem of cruise missile's performance test in complex electromagnetic environment, the whole trajectory simulation of cruise missile is researched in this paper. First, we analyze the role played by inertial navigation system(INS) in the process of cruise missile attack. Then, we build error model of inertial navigation system. At last, we design the whole trajectory simulation platform of cruise missile, which integrates trajectory programming module, inertial navigation calculation module, trajectory simulation module, simulation control module, terminal guidance module, and so on. Our research in this paper is an important technology accumulation, which is highly significant for performance test of cruise missile in complex electromagnetic environment.

Copyright

© 2013, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Yi Liu
AU  - Hai-bo Chen
AU  - Xu Sun
AU  - Yun-hong Li
PY  - 2013/03
DA  - 2013/03
TI  - The Whole Trajectory Simulation of Cruise Missile Based on Inertial Navigation Error Model
BT  - Proceedings of the 2nd International Conference on Computer Science and Electronics Engineering (ICCSEE 2013)
PB  - Atlantis Press
SP  - 251
EP  - 255
SN  - 1951-6851
UR  - https://doi.org/10.2991/iccsee.2013.65
DO  - 10.2991/iccsee.2013.65
ID  - Liu2013/03
ER  -