Academic Journal
ACOSS FIVE (Active Control of Space Structures). Phase 1A
| العنوان: | ACOSS FIVE (Active Control of Space Structures). Phase 1A |
|---|---|
| المؤلفون: | Auburn, Jean N, Breakwell, John A, Gupta, Narenda K, Lyons, Michael G, Margulies, Gabriel |
| المساهمون: | LOCKHEED MISSILES AND SPACE CO INC PALO ALTO CA PALO ALTO RESEARCH LAB |
| المصدر: | DTIC AND NTIS |
| سنة النشر: | 1982 |
| المجموعة: | Defense Technical Information Center: DTIC Technical Reports database |
| مصطلحات موضوعية: | Unmanned Spacecraft, CONTROL SYSTEMS, SPACE SURVEILLANCE, STABILITY, ACTUATORS, AUGMENTATION, CLOSED LOOP SYSTEMS, CONTROL THEORY, EQUATIONS, FLEXURAL PROPERTIES, INTEGRATED SYSTEMS, MATHEMATICAL MODELS, MECHANIZATION, OPTIMIZATION, REJECTION, SPACECRAFT COMPONENTS, STEADY STATE, TEST AND EVALUATION, VIBRATIONAL SPECTRA, ACOSS(Active Control of Space Structures), Control figured spacecraft, Spacecraft stability |
| الوصف: | The theory of steady-state disturbance rejection for large space structures is developed and tested analytically on a complex optical strawman configuration (CSDL Model 2). It is shown that active control is potentially feasible for micro-vibration stabilization of precision large structures. A number of brassboard experiments have been carried out to illustrate the theory and to address implementation and mechanization of active control systems. (Author) |
| نوع الوثيقة: | text |
| وصف الملف: | text/html |
| اللغة: | English |
| Relation: | http://www.dtic.mil/docs/citations/ADA116655 |
| الاتاحة: | http://www.dtic.mil/docs/citations/ADA116655 http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA116655 |
| Rights: | Approved for public release; distribution is unlimited. |
| رقم الانضمام: | edsbas.326A6AE2 |
| قاعدة البيانات: | BASE |
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