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A reusable rocket engine intelligen control
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Merrill, Walter C. Lorenzo, Carl F. |
| Copyright Year | 1988 |
| Description | An intelligent control system for reusable space propulsion systems for future launch vehicles is described. The system description includes a framework for the design. The framework consists of an execution level with high-speed control and diagnostics, and a coordination level which marries expert system concepts with traditional control. A comparison is made between air breathing and rocket engine control concepts to assess the relative levels of development and to determine the applicability of air breathing control concepts to future reusable rocket engine systems. |
| File Size | 632173 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880017017 |
| Archival Resource Key | ark:/13960/t4km4645k |
| Language | English |
| Publisher Date | 1988-07-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Control Systems Design Comparison Reusable Rocket Engines Air Breathing Engines Diagnosis Artificial Intelligence Expert Systems Propulsion System Configurations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
