S. Pines

发表

Sequential estimation when measurement function nonlinearity is comparable to measurement error.

W. Denham, S. Pines, 1966 .

Constants of the motion for optimum thrust trajectories in a central force field.

S. Pines, 1964 .

Aerodynamic Flutter Derivatives for a Flexible Wing with Supersonic and Subsonic Edges

Joseph L. Neuringer, John Dugundji, Samuel Pines, 1955 .

Comparison of Special Perturbation Methods in Celestial Mechanics with Application to Lunar Orbits

S. Pines, M. Payne, H. Wolf, 1962 .

Variation of parameters for elliptic and near circular orbits

S. Pines, 1961 .

Uniform Representation of the Gravitational Potential and its Derivatives

Samuel Pines, S. Pines, 1973 .

Two impulse trajectory optimization for the RAE-B orbit trim problem

S. Pines, M. Payne, J. Horsewood, 1972 .

Modifications of the Goddard Minimum Variance Program for the processing of real data

H. Wolf, J. Mohan, S. Pines, 1964 .

SEQUENTIAL ESTIMATION WHEN MEASUREMENT FUNCTION NONLINEARITY IS COMPARABLE TO MEASUREMENT ERROR

Walter Denham, Samuel Pines, W. Denham, 1965 .

Instability Analysis and Design of an Efficiently Tapered Plate Under Compressive Loading

S. Pines, 1947 .