Publication Date:
2016-06-07
Description:
The propulsion control requirements of supersonic aircraft are presented. Integration of inlet, engine, and airframe controls is discussed. The application of recent control theory developments to propulsion control design is described. Control component designs for achieving reliable, responsive propulsion control are also discussed.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
Proc. of the SCAR Conf., Part 1; p 399-415
Format:
application/pdf
Permalink