中国航空学报(英文版)2024,Vol.37Issue(12) :404-415.DOI:10.1016/j.cja.2024.07.003

Construction and kinematic performance analysis of a suspension support for wind tunnel tests of spinning projectiles based on wire-driven parallel robot with kinematic redundancy

Zhou ZHU Lu SHI Cong HE Lei ZHAN Qi LIN
中国航空学报(英文版)2024,Vol.37Issue(12) :404-415.DOI:10.1016/j.cja.2024.07.003

Construction and kinematic performance analysis of a suspension support for wind tunnel tests of spinning projectiles based on wire-driven parallel robot with kinematic redundancy

Zhou ZHU 1Lu SHI 1Cong HE 1Lei ZHAN 1Qi LIN1
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作者信息

  • 1. School of Aerospace Engineering,Xiamen University,Xiamen 361102,China
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Abstract

This paper presents a novel suspension support tailored for wind tunnel tests of spinning projectiles based on Wire-Driven Parallel Robot(WDPR),uniquely characterized by an SPM(Spinning Projectile Model)-centered mobile platform.First,an SPM-centered mobile platform,featuring two redundant and another unconstrained Degree of Freedom(DOF),and its suspension support mechanism are designed together,collectively constructing a WDPR endowed with kine-matic redundancy.Afterward,the kinematics of the mechanism,boundary equations for the redun-dant DOFs,and relevant kinematic performance indices are then proposed and formulated.The results from both prototype experiments and numerical assessments are presented.The capability of the support mechanism to replicate the complex coupled motions of the SPM is verified by the experimental results,while the proposed kinematics and boundary equations are also validated.Furthermore,it is revealed by numerical assessments that the redundant DOFs of the mobile plat-form exert a minimal impact on the kinematic performance of the suspension support.Finally,the optimal global attitude performance is obtained when these DOFs are set to zero if they are restricted to constants.However,local attitude performance can be further improved by the vari-able values.

Key words

Suspension support/Wire-Driven Parallel Robot(WDPR)/Spinning Projectile Model(SPM)/Wind tunnels/Kinematic performance analysis/Kinematic redundancy

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出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
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