
Accession Number : AD0748219
Title : ThreeDimensional, MinimumTime Flight Paths to a Point and onto a Line for a Supersonic Aircraft with a Maximum Mach Number Constraint.
Descriptive Note : Final rept.,
Corporate Author : STANFORD UNIV CA DEPT OF AERONAUTICS AND ASTRONAUTICS
Personal Author(s) : Parsons, Michael G. ; Bryson, Arthur E., Jr
Report Date : AUG 1972
Pagination or Media Count : 47
Abstract : Optimal control theory and the energystate approximation are used to determine the thrust, altitude, and bank angle programs for minimumtime flight paths of a supersonic aircraft from an initial energy, heading, and horizontal position to a specified final energy, heading, and point or line in a horizontal plane. Constraints on maximum and minimum thrust, stall angleofattack, maximum Mach number, maximum dynamic pressure, and maximum normal load factor are considered. The problem is restricted to those cases in which the flight path is long enough that the maximum Mach number is reached during the flight. Numerical results are presented for a typical supersonic aircraft capable of Mach 2.0 flight. (Author)
Descriptors : *FLIGHT PATHS, *SUPERSONIC AIRCRAFT, *FLIGHT CONTROL SYSTEMS, OPTIMIZATION, CYBERNETICS, MATHEMATICAL MODELS, EQUATIONS OF MOTION, FACTOR ANALYSIS, NUMERICAL METHODS AND PROCEDURES.
Subject Categories : Air Navigation and Guidance
Operations Research
Distribution Statement : APPROVED FOR PUBLIC RELEASE