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弹箭与制导学报 >

2020 , Vol. 40 >Issue 2: 29 - 31

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2020.02.007

基于ADAMS的无人机空中发射动力学仿真及分析

  • 张少江 1, 2 ,
  • 童小燕 1 ,
  • 姚磊江 1 ,
  • 张伟 1
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  • 1 西北工业大学无人机特种技术国防科技重点实验室, 西安 710072
  • 2 西北工业大学航空学院, 西安 710072

张少江(1994-),男,陕西铜川人,硕士,研究方向:飞行器设计与动力学仿真。

收稿日期: 2019-02-22

  网络出版日期: 2025-05-30

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Simulation and Analysis of Aerial Launch Dynamics of UAV Based on ADAMS

  • ZHANG Shaojiang 1, 2 ,
  • TONG Xiaoyan 1 ,
  • YAO Leijiang 1 ,
  • ZHANG Wei 1
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  • 1 Key of Laboratory of National Defense Science and Technology on UAV, Northwestern Polytechnical University, Xi’an 710072, China
  • 2 School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China

Received date: 2019-02-22

  Online published: 2025-05-30

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摘要

提出一种新型无人机空中旋转发射总体方案,并利用三维实体建模软件CATIA和动力学仿真软件ADAMS联合建立载机、无人机、发射架等的实体三维模型;对空中发射无人机过程进行了动力学仿真,得到了在给定发射初速度条件下无人机质心位移的变化曲线和无人机顶点与货舱底面垂向距离变化曲线,分析了空中发射无人机方案的可行性。分析结果表明:无人机在0.19 s可以出舱,且在整个过程中无人机与货舱不会发生碰撞,无人机可以安全离开载机。

关键词： ADAMS; 动力学仿真; 空中发射; 无人机

本文引用格式

张少江 , 童小燕 , 姚磊江 , 张伟 . 基于ADAMS的无人机空中发射动力学仿真及分析[J]. 弹箭与制导学报, 2020 , 40(2) : 29 -31 . DOI: 10.15892/j.cnki.djzdxb.2020.02.007

Abstract

In order to prove the feasibility of the UAV's overall air launch scheme, the three-dimensional solid model of the carrier, UAV and launcher is established by using the three-dimensional solid modeling software CATIA and dynamic simulation software ADAMS.The dynamic simulation of the process of launching UAV in the air is carried out, and the variation law of the UAV's center of mass displacement during the launching process is obtained, and the scheme of launching UAV in the air is analyzed.Feasibility, the results show that the scheme is feasible and the UAV can leave the carrier safely.

Key words： ADAMS; dynamics simulation; air launch; UAV

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