| contributor author | G. Y. Matsumoto | |
| contributor author | C. D. Mote | |
| date accessioned | 2017-05-09T01:23:32Z | |
| date available | 2017-05-09T01:23:32Z | |
| date copyright | December, 1972 | |
| date issued | 1972 | |
| identifier issn | 0022-0434 | |
| identifier other | JDSMAA-25995#330_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/159634 | |
| description abstract | An extension of the τ-decomposition method is used to predict the stability of a continuous system subjected to nonconservative loading. The technique is implemented through Ritz-finite element discretization. The stability of a flexible rocket (or beam) with a controlled orientation thrust vector (or follower force) is examined with respect to finite time delay in the control mechanism. Higher mode instabilities in the rocket are observed in the sample problem and are treated satisfactorily in the technique. Both buckling and flutter conditions are determined from eigenvalue trajectories in the complex plane. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Time Delay Instabilities in Large Order Systems With Controlled Follower Forces | |
| type | Journal Paper | |
| journal volume | 94 | |
| journal issue | 4 | |
| journal title | Journal of Dynamic Systems, Measurement, and Control | |
| identifier doi | 10.1115/1.3426616 | |
| journal fristpage | 330 | |
| journal lastpage | 334 | |
| identifier eissn | 1528-9028 | |
| keywords | Force | |
| keywords | Delays | |
| keywords | Rockets | |
| keywords | Stability | |
| keywords | Thrust | |
| keywords | Flutter (Aerodynamics) | |
| keywords | Buckling | |
| keywords | Mechanisms AND Eigenvalues | |
| tree | Journal of Dynamic Systems, Measurement, and Control:;1972:;volume( 094 ):;issue: 004 | |
| contenttype | Fulltext | |