Proceedings of the 2nd International Conference on Computer Science and Electronics Engineering

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

Authors
Yi Liu, Hai-bo Chen, Xu Sun, Yun-hong Li
Corresponding Author
Yi Liu
Available Online March 2013.
DOI
https://doi.org/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.
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This is an open access article distributed under the CC BY-NC license.

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Proceedings
Proceedings of the 2nd International Conference on Computer Science and Electronics Engineering
Part of series
Advances in Intelligent Systems Research
Publication Date
March 2013
ISBN
978-90-78677-61-1
DOI
https://doi.org/10.2991/iccsee.2013.65How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

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
PB  - Atlantis Press
UR  - https://doi.org/10.2991/iccsee.2013.65
DO  - https://doi.org/10.2991/iccsee.2013.65
ID  - Liu2013/03
ER  -