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.
Reusable Rocket Engine Intelligent Control
1988
11 pages
Report
No indication
English
A reusable rocket engine intelligent control
NTRS | 1988
|A reusable rocket engine intelligent control
AIAA | 1988
|A reusable rocket engine intelligen control
NTRS | 1988
|