Accession Number : AD0822874

Title :   APPLICATION OF OPTIMAL CONTROL THEORY TO VTOL FLIGHT CONTROL SYSTEM DESIGN.

Descriptive Note : Final rept. Jun 66-Apr 67,

Corporate Author : BELL AEROSYSTEMS CO BUFFALO NY

Personal Author(s) : Gaul, John W. ; Kaiser, Robert P. ; Onega, George T. ; DeCanio, Frank T.

Report Date : SEP 1967

Pagination or Media Count : 208

Descriptors :   *FLIGHT CONTROL SYSTEMS), (*VERTICAL TAKEOFF AIRCRAFT, ATTITUDE CONTROL SYSTEMS, RESEARCH PLANES, SHROUDED PROPELLERS, STABILIZATION SYSTEMS, HOVERING, LEVEL FLIGHT, AERODYNAMIC CHARACTERISTICS, PITCH(MOTION), YAW, MATHEMATICAL MODELS, OPTIMIZATION, DESIGN, HANDLING, MATHEMATICAL ANALYSIS, SPECIAL FUNCTIONS(MATHEMATICAL).

Subject Categories : V/STOL
      Research and Experimental Aircraft
      Numerical Mathematics

Distribution Statement : APPROVED FOR PUBLIC RELEASE