Experimental investigation of spacecraft in-flight disturbances and dynamic response

Journal of Spacecraft and Rockets

Volumn 34, Issue 2, 1997, Pages 199-204

  Woodard, Stanley E ^a,d,e   Lay, Richard R ^b,f   Jarnot, Robert F ^b,f   Gell, David A ^c,g  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^c UNIVERSITY OF MICHIGAN   (United States)

^d Structure Division   (United States)

^e AIAA   (United States)

^f Microwave Lidar Interferometer T   (United States)

^g and Space Sciences   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BENDING (DEFORMATION); DYNAMIC RESPONSE; ENERGY DISSIPATION; FLEXIBLE STRUCTURES; FRICTION; OSCILLATIONS; SPACE FLIGHT; SPACECRAFT INSTRUMENTS; VIBRATIONS (MECHANICAL);

SOLAR ARRAYS; UPPER ATMOSPHERE RESEARCH SATELLITE (UARS);

SATELLITE OBSERVATORIES;

EID: 0031102076     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3210     Document Type: Article

References (14)

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11. Zimbelman, D. F., "Thermal Elastic Shock and Its Effect on Topex Spacecraft Attitude Control," 14th Annual American Astronautical Society Guidance and Control Conf., Keystone, CO, Feb. 1991.
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