Optimal trajectory coordinate-multiplier systems with constant of the motion components.
Vector integral extension to optimal trajectory coordinate multiplier systems with constant of motion demonstrated for coast-arc problem
Miner, W. E.↗
Engineering topics
Miner, W. E.
Publications and source records attributed to Miner, W. E..
Necessary conditions for optimal lunar trajectories with discontinuous state variables and intermediate point constraints.
Guidance regime for optimal multistage lunar trajectory derived by applying calculus of variations to generalized Bolza problem
Andrus, J. F.↗
The equations of motion for optimized propelled flight expressed in Delaunay and Poincare variables and modifications of these variables
Development of equations of motion in canonical form equivalent to forms of Delaunay and Poincare
Miner, W. E.↗
The Hamilton-Jacobi method applied to the low-thrust trajectory problem.
Spacecraft optimum low thrust trajectory analyzed by Hamilton-Jacobi perturbation theory, obtaining canonic constants of motion
Miner, W. E.↗
Necessary conditions for optimal lunar trajectories with discontinuous state variables and intermediate point constraints
Necessary conditions for optimal lunar trajectories with discontinuous state variables and intermediate point constraints
TRAJECTORY OPTIMIZATION↗
On studies in the field of space flight and guidance theory progress report no. 4 <20 dec. 1962 - 18 jul. 1963<
Trajectories, orbital calculations, and adaptive guidance
ORBIT CALCULATION↗
A VARIATIONAL LAUNCH WINDOW STUDY
Obtention of a launch window, as a function of allowable performance loss, for placing a saturn v in a circular orbit in a prespecified space-fixed plane
ORBITAL MECHANICS↗
LAUNCH WINDOW STUDIES EMPLOYING VARIATIONAL CALCULUS TO DETERMINE OPTIMUM THREE DIMENSIONAL TRAJECTORIES LEADING TO INJECTION INTO A SPACE-FIXED CIRCULAR ORBIT
Determination of optimum 3-dimensional trajectories to inject a saturn c-5 rocket into a space-fixed circular orbit
SPACECRAFT TRAJECTORY↗
LAUNCH WINDOW STUDIES EMPLOYING VARIATIONAL CALCULUS TO DETERMINE OPTIMUM THREE DIMENSIONAL TRAJECTORIES LEADING TO INJECTION INTO A SPACE-FIXED CIRCULAR ORBIT
Determination of optimum trajectories leading to circular orbits
CIRCULAR ORBIT↗
STUDIES IN THE FIELDS OF SPACE FLIGHT AND GUIDANCE THEORY. INTRODUCTION
Guidance systems and flight optimization theory for space flight
FLIGHT OPTIMIZATION↗
The varicentric method of space flight calculation with introduction of the ephemerides progress report no. 1
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Miner, W. E.↗