原文传递
Optimization of Second Fault Detection Thresholds to Maximize Mission Probability of Success.
| 题名： | Optimization of Second Fault Detection Thresholds to Maximize Mission Probability of Success. |
| 作者： | Anzalone, E. |
| 关键词： | Space launch system (sls), Design optimization, Fault detection, Probability theory, Complex systems, Navigation, Specifications, Tolerances (mechanics), Payloads, Accuracy, Computerized simulation, Monte carlo method |
| 摘要： | No abstract available |
| 报告类型： | 科技报告 |
相关文献
- SPACE PROPULSION SYSTEM PHASED-MISSION PROBABILITY ANALYSIS USING CONVENTIONAL PRA METHODS
- Classification of Aircraft Maneuvers for Fault Detection
- Simulation and Optimization at Kansas City Southern Railway: Equipping Management for Success.
- Electrodynamic Dust Shield for Space Applications.
- Instructional Design Reference Mission for Search and Rescue Operations.
- MARKETING ETC : PLANNING FOR SUCCESS.
检索历史
应用推荐
