| contributor author | Chris S. Schulz | |
| contributor author | Norman M. Wereley | |
| contributor author | Donald L. Kunz | |
| date accessioned | 2017-05-09T00:43:03Z | |
| date available | 2017-05-09T00:43:03Z | |
| date copyright | January, 2011 | |
| date issued | 2011 | |
| identifier issn | 0022-0434 | |
| identifier other | JDSMAA-26541#011001_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/145740 | |
| description abstract | System identification techniques are often used to determine the parameters required to define a model of a linear time invariant (LTI) system. The Cramer–Rao bound can be used to validate those parameters in order to ensure that the system model is an accurate representation of the system. Unfortunately, the Cramer–Rao bound is only valid for LTI systems and is not valid for linear time periodic (LTP) systems such as a helicopter rotor in forward flight. This paper describes an extension of the Cramer–Rao bound to LTP systems and demonstrates the methodology for a simple LTP system. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Cramer–Rao Bound Development for Linear Time Periodic Systems | |
| type | Journal Paper | |
| journal volume | 133 | |
| journal issue | 1 | |
| journal title | Journal of Dynamic Systems, Measurement, and Control | |
| identifier doi | 10.1115/1.4002104 | |
| journal fristpage | 11001 | |
| identifier eissn | 1528-9028 | |
| keywords | Rotors | |
| keywords | Signals | |
| keywords | Blades | |
| keywords | Locks (Waterways) | |
| keywords | Frequency response | |
| keywords | Flight | |
| keywords | Errors AND Electromagnetic pulse | |
| tree | Journal of Dynamic Systems, Measurement, and Control:;2011:;volume( 133 ):;issue: 001 | |
| contenttype | Fulltext | |
