| タイトル | NASA IVHM Technology Experiment for X-vehicles (NITEX) |
| 本文（外部サイト） | http://hdl.handle.net/2060/20020008402 |
| 著者（英） | Sandra, Hayden; Bajwa, Anupa |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 2001-01-01 |
| 言語 | eng |
| 内容記述 | The purpose of the NASA IVHM Technology Experiment for X-vehicles (NITEX) is to advance the development of selected IVHM technologies in a flight environment and to demonstrate the potential for reusable launch vehicle ground processing savings. The technologies to be developed and demonstrated include system-level and detailed diagnostics for real-time fault detection and isolation, prognostics for fault prediction, automated maintenance planning based on diagnostic and prognostic results, and a microelectronics hardware platform. Complete flight The Evolution of Flexible Insulation as IVHM consists of advanced sensors, distributed data acquisition, data processing that includes model-based diagnostics, prognostics and vehicle autonomy for control or suggested action, and advanced data storage. Complete ground IVHM consists of evolved control room architectures, advanced applications including automated maintenance planning and automated ground support equipment. This experiment will advance the development of a subset of complete IVHM. |
| NASA分類 | Technology Utilization and Surface Transportation |
| 権利 | No Copyright |
|
