타이틀 |
The Digital Twin Paradigm for Future NASA and U.S. Air Force Vehicles |
저자 |
Glaessgen, Edward H.;; Stargel, D. S. |
Keyword |
AEROSPACE VEHICLES;; COMPUTER GRAPHICS;; CRACKING (FRACTURING); DIGITAL TECHNIQUES;; DYNAMIC STRUCTURAL ANALYSIS;; FLIGHT SAFETY;; FRACTURE MECHANICS;; MECHANICAL PROPERTIES;; MILITARY AIRCRAFT;; MULTISCALE MODELS;; NONDESTRUCTIVE TESTS;; RELIABILITY ANALYSIS;; SITUATIONAL AWARENESS;; STATISTICAL DISTRIBUTIONS;; STRESS INTENSITY FACTORS;; SYSTEMS HEALTH MONITORING;; SYSTEMS INTEGRATION |
URL |
http://hdl.handle.net/2060/20120008178 |
보고서번호 |
AIAA Paper 2012-1818 |
발행년도 |
2012 |
출처 |
NTRS (NASA Technical Report Server) |
ABSTRACT |
Future generations of NASA and U.S. Air Force vehicles will require lighter mass while being subjected to higher loads and more extreme service conditions over longer time periods than the present generation. Current approaches for certification, fleet management and sustainment are largely based on statistical distributions of material properties, heuristic design philosophies, physical testing and assumed similitude between testing and operational conditions and will likely be unable to address these extreme requirements. To address the shortcomings of conventional approaches, a fundamental paradigm shift is needed. This paradigm shift, the Digital Twin, integrates ultra-high fidelity simulation with the vehicle s on-board integrated vehicle health management system, maintenance history and all available historical and fleet data to mirror the life of its flying twin and enable unprecedented levels of safety and reliability. |