惯性滑翔阶段攻角对电视制导弹制导精度的影响研究

2012 International Conference on Computer Science and Information Processing (CSIP) Pub Date : 2012-09-24 DOI:10.1109/CSIP.2012.6309096

Xiao Sheng, Zhi-min Qi, Ming Hou, Hanjun Yu

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引用次数: 0

摘要

建立了电视制导弹的刚体弹道模型，分析了攻角对电视制导弹制导精度的影响。基于MATLAB仿真了初始条件下惯性制导滑翔相位轨迹。得到攻角和由攻角引起的误差。提出了一种校正平衡攻角消除误差的方法，为提高电视制导炮弹的制导精度提供了理论依据。

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Study on influence of angle-of-attack on TV-guided Shell guidance precision in inertial glide phase

Built up the rigid body trajectory model of TV-guided shell, and analyzed the effect of angle-of-attack on guidance precision of TV-guided shell. Simulated trajectory of inertial guidance glide phase in an initial condition based on MATLAB. Get angle-of-attack and the error caused by angle-of-attack. Advance a way of correcting balance angle-of-attack to eliminate error, which provides a theoretical foundation for improving TV-guided Shell guidance precision.

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2012 International Conference on Computer Science and Information Processing (CSIP)

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