SCOPUS 정보 검색 플랫폼

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 6, Issue , 2003, Pages 3971-3982

An articulated motion and vibration isolator for spacecraft

(4) Murphey, Thomas W a Botke, Matthew b Blankinship, Ross M c Hague, Nick T d

a UNIVERSITY OF CAMBRIDGE (United Kingdom)

b NORTHROP GRUMMAN CORPORATION (United States)

c CSA ENGINEERING (United States)

d AIR FORCE RESEARCH LABORATORY (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION CONTROL; CONTROL SYSTEM SYNTHESIS; DEGREES OF FREEDOM (MECHANICS); EQUATIONS OF MOTION; HARMONIC ANALYSIS; KINEMATICS; MOTION CONTROL; VIBRATION CONTROL;

MOTION ISOLATOR; ROTATIONAL DEGREES OF FREEDOM; TRANSLATIONAL DEGREES OF FREEDOM; VIBRATION ISOLATOR;

SPACECRAFT;

EID: 0041508817 PISSN: 02734508 EISSN: None Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper

Times cited : (3)

References (10)

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2
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- Thin-film and crystalline solar cell array system performance comparisons
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3
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- NASA/CP-2002-211506
- Botke, M., Murphy, D., Murphey, T., Sorensen, P., "Zero Deadband, Multiple Strut Synchronized Hinge for Deployable Structures," Proceedings of the 36th Aerospace Mechanisms Symposium, May 2002, NASA/CP-2002-211506
- Proceedings of the 36th Aerospace Mechanisms Symposium, May 2002
- Botke, M.¹ Murphy, D.² Murphey, T.³ Sorensen, P.⁴

4
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5
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- McGraw-Hill, Inc.
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- Young, W.C.¹

6
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7
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- The Tiffen Company, LLC
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8
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9
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10
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.