## XI non-linear dynamic behaviour, sufficient complexity and multiple faults. First, quantitative models for normal and faulty behaviour of the system were described. These models were used for a simulation which was built up by software components and integrated into the BEHAVIOR workbench. Fina
A knowledge based aircraft-gate assignment advisor
โ Scribed by Y.Y. Su; K. Srihari
- Publisher
- Elsevier Science
- Year
- 1993
- Tongue
- English
- Weight
- 414 KB
- Volume
- 25
- Category
- Article
- ISSN
- 0360-8352
No coin nor oath required. For personal study only.
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