方位连续旋转垂直发射飞行器仿真方法研究

系统仿真学报 ›› 2016, Vol. 28 ›› Issue (6): 1329-1336.

方位连续旋转垂直发射飞行器仿真方法研究

刘成生¹, 张卿²

1.92941部队93分队,辽宁葫芦岛 125001;
2.北京机电工程研究所,北京 100074

收稿日期:2014-11-05 修回日期:2015-06-19 出版日期:2016-06-08 发布日期:2020-06-08
作者简介:刘成生(1965-),男,山东宁津,硕士,高工,研究方向为导弹武器系统试验总体技术;张卿(1981-),女,河北邢台,硕士,高工,研究方向为飞行器系统仿真技术。

Method of Hardware-in-the-Loop (HWIL) Simulation for Pose Movement of Vertical Launching Aerocraft With Continuous Rotation in Yaw

Liu Chengsheng¹, Zhang Qing²

1. Unit 92941 of PLA, Huludao 125001, China;
2. Beijing Electro-Mechanical Engineering Institute, Beijing 100074, China

Received:2014-11-05 Revised:2015-06-19 Online:2016-06-08 Published:2020-06-08

摘要/Abstract

摘要： 在分析三轴仿真转台模拟方位可连续旋转的垂直发射飞行器姿态运动缺陷的基础上,提出一种能够模拟飞行器俯仰、滚动姿态不小于±180°变化范围并且航向姿态变化无限大的四轴仿真转台方案,进行四轴转台结构布局分析和控制建模,并设计基于“切换运动机制”的四轴协调运行控制规律,完成转台控制过程中的平滑切换措施设计及仿真验证。证明了四轴仿真转台及其协调运行控制方案,为方位连续旋转的垂直发射飞行器全程飞行姿态运动的模拟提供了一种连续、实时、高效的仿真方法。

关键词: 垂直发射, 四轴仿真转台, 切换运动机制, 协调运行控制规律

Abstract: There are defects in the pose movement simulation of vertical launching aerocraft which can circumrotate continuously in yaw with three -axis flight motion simulator. Based on analysis of these defects, a four-axis project which could be applied to the situation of the changing range of vehicle pitch pose and vehicle roll attitude more than ±180° and the changing range of vehicle course pose towards infinite greatness was proposed. The structure of the four-axis flight motion simulator was analyzed and the control model was made. Above all, a four-axis concerted control law was designed with" switching movement mechanism", and a smooth switch measure in the control process of flight motion simulator was designed too, then the result was validated with simulation. A continuous, real-time and high-efficient simulation method for the pose movement of vertical launching aerocraft which could circumrotate continuously in yaw was confirmed.

Key words: vertical launching, four-axis flight motion simulator, switching movement mechanism, concerted control law

中图分类号:

V448.22

刘成生, 张卿. 方位连续旋转垂直发射飞行器仿真方法研究[J]. 系统仿真学报, 2016, 28(6): 1329-1336.

Liu Chengsheng, Zhang Qing. Method of Hardware-in-the-Loop (HWIL) Simulation for Pose Movement of Vertical Launching Aerocraft With Continuous Rotation in Yaw[J]. Journal of System Simulation, 2016, 28(6): 1329-1336.

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