Accession Number : AD0832009

Title :   TRAJECTORY OPTIMIZATION BY METHOD OF STEEPEST DESCENT. VOLUME II. USER'S MANUAL.

Descriptive Note : Final rept.,

Corporate Author : MCDONNELL AIRCRAFT CO ST LOUIS MO

Personal Author(s) : Schmidt,Harvey E. ; Helgason,Richard V. ; Witherspoon,James T. ; Geib,Kenneth E.

Report Date : APR 1968

Pagination or Media Count : 273

Descriptors :   (*GUIDED MISSILE TRAJECTORIES, OPTIMIZATION), (*COMPUTER PROGRAMMING, GUIDED MISSILE TRAJECTORIES), DESCENT TRAJECTORIES, STEEPEST DESCENT METHOD, STAGNATION POINT, RANGE(DISTANCE), ORBITS, ATMOSPHERE MODELS, AERODYNAMIC HEATING, INSTRUCTION MANUALS, ENERGY, WIND, VELOCITY, THRUST, CONTROL SYSTEMS, ERRORS, APPROXIMATION(MATHEMATICS), EQUATIONS OF MOTION, PERTURBATION THEORY, ITERATIONS, COMPUTER PROGRAMS

Subject Categories : Computer Programming and Software
      Guided Missile Dynam, Config & Cntrl Surfaces

Distribution Statement : APPROVED FOR PUBLIC RELEASE