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| 003 | MiAaHDL | ||
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| 008 | 220427s1991 ohua bt f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡a(MiU)99187625243606381 |
| 035 | ⊔ | ⊔ | ‡asdr-miu.99187625243606381 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)1312743124 |
| 035 | ⊔ | ⊔ | ‡a(GWLA)gwla on1312743124 |
| 040 | ⊔ | ⊔ | ‡aTRAAL ‡beng ‡erda ‡cTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/57:91-3058 |
| 100 | 1 | ⊔ | ‡aRao, S. S., ‡eauthor. |
| 245 | 1 | 0 | ‡aRobustness improvement of actively controlled structures through integrated structural/control design / ‡cS.S. Rao and T.S. Pan. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bFliight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, ‡c1991 |
| 300 | ⊔ | ⊔ | ‡a162 pages : ‡billustrations ; ‡c28 cm |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aAFWAL-TR (Air Force Wright Aeronautical Laboratories) ; ‡v91-3058 |
| 500 | ⊔ | ⊔ | ‡a"Final Report for Period October 1987 - May 1991." |
| 500 | ⊔ | ⊔ | ‡a"May 1991." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (pages 152-162). |
| 520 | ⊔ | ⊔ | ‡aThe problem of structural and control design of flexible structures is considered. Three major topics are investigated. The first topic deals with the dual passive/active control design for flexible structures. The interacting sub-structure decentralized control approach is developed for large flexible structures to eliminate the spillover problem and reduce the model size for controller margin and robustness of controlled flexible structures. The second topic considers the robustness improvement for controlled flexible structures through structure modifications. The stability and engineering performance robustness indices are defined. The integrated structural/control design problem is considered as a multiobjective optimization problem in which three objectives- structural weight, stability robustness index and performance robustness index- are considered for minimization. The third topic involves the study of the actuator/sensor location selection problem. The sequential-best-adding, penalty function method and the genetic algorithm are considered. |
| 536 | ⊔ | ⊔ | ‡aResearch supported by the United States Air Force Flight Dynamics Directorate, and performed by School of Mechanical Engineering, Purdue University, West Lafayette, Indiana, under Contract No. ‡bF33615-87-C-3256. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aSpace vehicles ‡xControl systems. |
| 650 | ⊔ | 0 | ‡aSpace vehicles ‡xDesign and construction. |
| 700 | 1 | ⊔ | ‡aPan, T. S., ‡eauthor. |
| 710 | 2 | ⊔ | ‡aWright Laboratory (Wright-Patterson Air Force Base, Ohio), ‡eissuing body. |
| 710 | 2 | ⊔ | ‡aPurdue University. ‡bSchool of Mechanical Engineering, ‡esponsor. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
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