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Simulation modeling for long duration spacecraft control systems
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bavuso, Salvatore J. Boyd, Mark A. |
| Copyright Year | 1993 |
| Description | The use of simulation is described and it is contrasted to analytical solution techniques for evaluation of analytical reliability models. The role importance sampling plays in simulation of models of this type was also discussed. The simulator tool used for our analysis is described. Finally, the use of the simulator tool was demonstrated by applying it to evaluate the reliability of a fault tolerant hypercube multiprocessor intended for spacecraft designed for long duration missions. The reliability analysis was used to highlight the advantages and disadvantages offered by simulation over analytical solution of Markovian and non-Markovian reliability models. |
| File Size | 663193 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940021785 |
| Archival Resource Key | ark:/13960/t2w42p68c |
| Language | English |
| Publisher Date | 1993-12-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Fault Tolerance Hypercube Multiprocessors Spacecraft Reliability Reliability Analysis Spacecraft Control Mathematical Models Computerized Simulation Simulators Long Duration Space Flight Fault Trees Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
