锥齿轮推杆式弹头偏转机构的设计与仿真

胡寒栋; 谷良贤; 梁毅辰; 孙晓峰

doi:10.13433/j.cnki.1003-8728.2015.0732

锥齿轮推杆式弹头偏转机构的设计与仿真

doi: 10.13433/j.cnki.1003-8728.2015.0732

1.
西北工业大学航天飞行动力学技术重点实验室, 西安 710072

详细信息

作者简介:
胡寒栋（1993-），硕士研究生，研究方向为飞行器总体设计、气动和结构，986183389@qq.com

通讯作者:
谷良贤，教授，博士，gulx@nwpu.edu.cn

计量
- 文章访问数: 207
- HTML全文浏览量: 39
- PDF下载量: 10
- 被引次数: 0
出版历程
- 收稿日期: 2013-10-30
- 刊出日期: 2015-07-05

Design and Simulation of Hand-spike Nose Deflecting Mechanism for Guide-screw

1.
National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical University, Xi'an 710072, China

摘要

摘要: 分析现有偏转驱动机构缺点，总结了弹头偏转机构的设计要求，并针对该要求设计出一种锥齿轮推杆式偏转机构；接着推导了锥齿轮推杆式偏转机构弹头偏角和电动机转动参数的关系。建立虚拟样机并结合ADAMS与MATLAB/Simulink开展联合仿真，证明锥齿轮推杆式驱动机构具有精度高、响应速度快、可实现较大角度偏转等优点，能够满足偏转弹头控制的要求。
- 偏转弹头控制技术 /
- 机构 /
- 设计 /
- 仿真 /
- 动力学特性 /
- 锥齿轮推杆式
Abstract: The existing deflection mechanisms' characteristics are analyzed, the requirements of the nose deflection mechanism is summarized, an efficient mechanism programs-a Screw-Spike nose deflecting mechanism is designed. The relationship between the deflecting angles of nose and the rotation of motors is deduced. Virtual prototype is established and coupled simulating the ADAMS-MATLAB/Simulink. The advantages of high precision, fast response, larger achievable deflection angles meets the requirements of deflectable nose control.
- acoustic noise /
- bevel-gear hand-spike /
- brushless DC motors /
- computer simulation /
- computer software /
- control

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参考文献(17)

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