CONTACT-IMPACT ANALYSIS OF DEPLOYABLE SPACE SYSTEMS-Reference-Cited by-同舟云学术

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CONTACT-IMPACT ANALYSIS OF DEPLOYABLE SPACE SYSTEMS

Published:1993-04-19 Issue: Volume: Page:
ISSN:
Container-title:34th Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

WU SHIH-CHIN¹,CHEN GUN-SHING²

Affiliation:

1. LOCKHEED ENGINEERING AND SCIENCE COMPANY, HAMPTON, VA

2. JET PROPULSION LABORATORY, PASADENA, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-1544

Reference23 articles.

1. 11) Substituting the results of Eqs. 3.6-3.11 into Eq. 3.4, one obtains

2. (tI +0)=q(t1-0)+Aq and the position obtained from prior integration as initial conditions to restart integration of Eq. 2.6. This procedure yields a unique solution of the equations of motion, including the effect of the impact event.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Influence of thrust modulation on a satellite with flexible non-latching booms;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2022-11-16

2. Computational strategies for flexible multibody systems;Applied Mechanics Reviews;2003-11-01

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