| contributor author | B. Dobrotin | |
| date accessioned | 2017-05-08T23:20:42Z | |
| date available | 2017-05-08T23:20:42Z | |
| date copyright | February, 1985 | |
| date issued | 1985 | |
| identifier issn | 1087-1357 | |
| identifier other | JMSEFK-27712#22_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/100129 | |
| description abstract | Autonomy is used on spacecraft for minimizing operational cost and providing onboard failure response. System studies have been performed to provide spacecraft design criteria. This paper presents the design drivers and recommended design criteria for the Data Handling Subsystem (DHS). The impact of interfacing spacecraft subsystems, as well as alternate solutions, is discussed. The importance of establishing detail processing requirements through a Failure Modes and Effects Analysis (FMEA) is addressed and related to various spacecraft computer capabilities. A prioritized list of DHS design topics is included. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Implementing Spacecraft Autonomy | |
| type | Journal Paper | |
| journal volume | 107 | |
| journal issue | 1 | |
| journal title | Journal of Manufacturing Science and Engineering | |
| identifier doi | 10.1115/1.3185959 | |
| journal fristpage | 22 | |
| journal lastpage | 25 | |
| identifier eissn | 1528-8935 | |
| keywords | Space vehicles | |
| keywords | Design | |
| keywords | Homeland security | |
| keywords | Failure | |
| keywords | Failure mode and effects analysis AND Computers | |
| tree | Journal of Manufacturing Science and Engineering:;1985:;volume( 107 ):;issue: 001 | |
| contenttype | Fulltext | |
