Anderson et al., 1999 - Google Patents
Satellite ultraquiet isolation technology experiment (SUITE): electromechanical subsystemsAnderson et al., 1999
- Document ID
- 14686122260790992439
- Author
- Anderson E
- Evert M
- Glaese R
- Goodding J
- Pendleton S
- Camp D
- Fumo J
- Jessen M
- Cobb R
- Erwin R
- Jensen J
- Publication year
- Publication venue
- Smart Structures and Materials 1999: Industrial and Commercial Applications of Smart Structures Technologies
External Links
Snippet
Spacecraft carry instruments and sensors that gather information from distant points, for example, from the Earth's surface several hundred kilometers away. Small vibrations on the spacecraft can reduce instrument effectiveness significantly. Vibration isolation system are …
- 238000002955 isolation 0 title abstract description 87
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Anderson et al. | Satellite ultraquiet isolation technology experiment (SUITE) | |
Cobb et al. | Vibration isolation and suppression system for precision payloads in space | |
Grodsinsky et al. | Survey of active vibration isolation systems for microgravity applications | |
Spanos et al. | A soft 6-axis active vibration isolator | |
KR101441628B1 (en) | Gyrodyne and device for assembly thereof | |
US5327061A (en) | Force (torque) nulling inertially servoed structural interface | |
US6454215B1 (en) | Spacecraft architecture for disturbance-free payload | |
Davis et al. | Second-generation hybrid D-strut | |
US6340137B1 (en) | Moment control unit for spacecraft attitude control | |
McMickell et al. | Optical payload isolation using the miniature vibration isolation system (MVIS-II) | |
Anderson et al. | Satellite ultraquiet isolation technology experiment (SUITE): electromechanical subsystems | |
US5419528A (en) | Vibration isolation mounting system | |
Johnson et al. | Softride vibration and shock isolation systems that protect spacecraft from launch dynamic environments | |
JP2952257B2 (en) | Attenuation instrument kinematic mount | |
Flint et al. | Active/passive counter-force vibration control and isolation systems | |
Anderson et al. | Ultraquiet platform for active vibration isolation | |
Quenon et al. | Miniature vibration isolation system for space applications | |
Bushnell et al. | Active rack isolation system development for the International Space Station | |
Nye et al. | Performance of active vibration control technology: the ACTEX flight experiments | |
Whorton | Microgravity vibration isolation for the International Space Station | |
Whorton | G-LIMIT-A microgravity vibration isolation system for the International Space Station | |
Brackett et al. | Miniature vibration isolation system (MVIS) | |
Sullivan et al. | Experiences with smart structures for on-orbit vibration isolation | |
Ryan et al. | The dynamic phenomena of a tethered satellite: NASA's first Tethered Satellite Mission, TSS-1 | |
Abhilash et al. | Passive Flexural Ring Micro-Vibration Isolator for Spacecraft Actuators |