국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	SUPERSONIC FLIGHT TEST RESULTS OF A PERFORMANCE SEEKING CONTROL ALGORITHM ON A NASA F-15 AIRCRAFT
저자	John S. Orme and Timothy R. Conners
Keyword	n.a.
URL	http://www.dfrc.nasa.gov/DTRS/1994/PDF/H-1985.pdf
보고서번호	AIAA-94-3210
발행년도	1994
출처	NASA Dryden Flight Research Center
ABSTRACT	A model-based, adaptive control algorithm called Performance Seeking Control (PSC) has been flight tested on an F-15 aircraft. The algorithm attempts to optimize performance of the integrated propulsion system during steady-state engine operation. The final phase of a 3-year PSC flight test program is described in this paper. Previous studies of use of PSC on the F-15 airplane show improvement in propulsion system performance. Because these studies were conducted using one of two F-15 engines, the full effect on aircraft performance was not measured. During the most recent studies, both engines were optimized to demonstrate the full effect of PSC propulsion system optimization on aircraft performance. Results were gathered over the 1-g supersonic envelope demonstrating benefits of the integrated control approach. Quantitative flight results illustrating the PSC method for deriving benefits from the F-15 integrated propulsion system for Mach numbers up to 2 are also presented.