Six-axis vibration isolation system using soft actuators and multiple sensors

Journal of Spacecraft and Rockets

Volumn 39, Issue 2, 2002, Pages 206-212

  Thayer, Doug ^a   Campbell, Mark ^a   Vagners, Juris ^a   Von Flotow, Andrew ^b  

^a UNIVERSITY OF WASHINGTON   (United States)

^b Hood Technology Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; DEGREES OF FREEDOM (MECHANICS); ELASTOMERS; SENSORS; STIFFNESS; VIBRATION CONTROL;

ELASTOMERIC FLEXURES; SPACE BASED SYSTEMS; SPACEBORNE INTERFEROMETRY; VOICE COIL ACTUATOR;

SPACE RESEARCH;

EID: 0036493633     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3821     Document Type: Article

References (14)

1. A platform with six degrees of freedom
2. Six degree of freedom active isolation using the Stewart platforms
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4. Active vibration isolation with stiff actuators and inertial sensors
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6. Satellite ultraquiet isolation technology experiment (SUITE)
7. Hybrid active/passive actuator for spacecraft vibration isolation suppression
8. A soft 6-axis active vibration isolator
9. Shaping the transmissibility for six-axis active vibration isolators
10. Active vibration isolation for precision space structures
11. Frequency shaped cost functionals: Extension of linear quadratic Gaussian design methods