Finite element analysis of maneuvering spacecraft truss structures

DOI10.1016/0045-7949(89)90316-7zbMATH Open0698.73052OpenAlexW2082928869MaRDI QIDQ3476388

E. R. Christensen

Publication date: 1989

Published in: Computers & Structures (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7949(89)90316-7

zbMATH Keywords

principle of virtual worktrapezoidal rulegoverning equations of motioninertial reference frameiterative direct numerical integration schemelarge angle slew maneuverslarge nonsteady translational and rotational motionsmomentum conservation principlesset of nonlinear second order matrix differential equationstime response of flexible spacecraft truss structures

Mathematics Subject Classification ID

Finite element methods applied to problems in solid mechanics (74S05)

Related Items (5)

Methodology of Structural–Functional Synthesis for the Small Spacecraft Onboard System Appearance ⋮ Integrated design of space structures using lattice plate finite elements ⋮ Space-variant finite element reliability analysis ⋮ Построение механических аналогов подконструкций с учетом действующих на них активных сил ⋮ Multibody dynamic simulation of the next generation space telescope using finite elements and fuzzy sets

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