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MATHEMATICS OF DYNAMIC PROGRAMMING MATRIX
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accuracy check aircraft constants altitude and velocity Altitude at d2 Altitude at Distance altitude dependent density Altitude feet altitude h Appendix arrival point BEECHCRAFT SUPER KING Candidate Altitude climb density altitude departure point Departure Weight derived as Ground distance elements distance index distance node Distance Point dynamic programming EQUATION FOR TURBOCHARGED EQUATION FOR TURBOPROP FBREF FIGURE A-7 flight level flight path flight planning aid fuel burn equation fuel burn model fuel consumption fuel efficient Golden Eagle Ground Distance Ground Velocity FIGURE increment inflight update input ISA CONDITIONS King Air 200 matrix maximum Minicomputer minimum fuel nodal point O'LZ OOLX optimal path optimum output path profile performance constraints power setting PRELIMINARY FUNCTIONAL CONCEPT pressure altitude previously defined programmable calculator segment solution Super King Air TABLE B-2 technique Teledyne Continental Motors thrust trip TURBOCHARGED PISTON turbojet velocity and altitude Velocity knots waypoint wind component winds and temperatures