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报告编号NASA-TM-87617, NAS 1.15:87617
来源IDNTRS_Document_ID: 19860019509
Nonlinear Dynamic Analysis of Deploying Flexible Space Booms
Mcgowan, P. E.; Housner, J. M.
英文摘要A fundamental investigation of the planar deployment and lock-up of two flexible boom type appendages which have attached tip masses and are connected to a central rigid body through a rotational spring is presented. Nondimensional parameters are identified and it is shown that, in general, the solution depends only on two mass ratios and one nondimensional stiffness parameter. Results are presented for boom tip deflections, deployment time and root moments at lock-up. A threshold value of the nondimensional stiffness parameter is identified beyond which boom deflections become large. Also, a thorough examination of the effect of nonlinear terms in the equations governing the deployment phase is performed. Nonlinear terms in the deployment equations due to kinematics and structural deformation are required to predict more accurately boom deflections, but retention of an inconsistent set of nonlinear terms leads to erroneous results. In particular, retaining nonlinear kinematic terms while neglecting nonlinear structural terms can produce inaccurate results even below the threshold stiffness value.
英文关键词BOOMS (EQUIPMENT) DEPLOYMENT DYNAMIC STRUCTURAL ANALYSIS FLEXIBLE BODIES KINEMATIC EQUATIONS LARGE SPACE STRUCTURES DEFLECTION DEFORMATION EQUATIONS OF MOTION MASS RATIOS PARAMETER IDENTIFICATION RIGID MOUNTING STIFFNESS MATRIX STRUCTURAL ANALYSIS
出版年1985
报告类型Technical Report
语种英语
国家美国
URLhttp://hdl.handle.net/2060/19860019509
资源类型科技报告
条目标识符http://119.78.100.177/qdio/handle/2XILL650/259037
推荐引用方式
GB/T 7714
Mcgowan, P. E.,Housner, J. M.. Nonlinear Dynamic Analysis of Deploying Flexible Space Booms,1985.
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