The Integrated Propulsion Control System (IPCS) demonstrates control of an entire supersonic propulsion module - inlet, engine afterburner, and nozzle - with an HDC 601 digital computer. The program encompasses the design, build, qualification, and flight testing of control modes, software, and hardware. The flight test vehicle is an F-111E airplane. The L.H. inlet and engine will be operated under control of a digital computer mounted in the weapons bay. A general description and the current status of the IPCS program are given.
IPCS implications for future supersonic transport aircraft
1976-08-01
Conference paper
No indication
English
Engineering Index Backfile | 1962
|Emerald Group Publishing | 1961
Engineering Index Backfile | 1961
Engineering Index Backfile | 1960