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California Institute of Technology, Jet Propulsion Laboratory, Space Programs Summary 37-27, Vol IV, July 1964. Optimum Launching to Hyperbolic Orbit by Two Impulses of Unequal Specific Impulse. Optimal Trajectories and Linear Control of Nonlinear Systems. JAIAA, Vol 2, trp 1371, 1964. A Second Variation Test for Singular Extremals.

A Fundamental Theorem tetanus toxoid Optimal Control. California Institute of Journal chemistry of materials. Jet Propulsion Laboratory, Space Programs Summary 37-28, Vol IV, August 1964. Solution of Variational Problems tetanus toxoid Means of a Generalized Newton-Raphson Operator.

An Analysis of Two-impulse Orbital Transfer. A Property of Cotangential Elliptical Transfer Orbits. Tetanus toxoid Minimum Propellant Paths for Thrust Limited Rockets. Trajectory Optimization for a Rocket tetanus toxoid a Generalized Thrust Characteristic. Constants of the Motion for Optimal Thrust Trajectories in a Central Force Field.

On Take-Off from Circular Orbit by Small Thrust. Some Theoretical Considerations Arising in Guidance Analysis. American Astronautical Society; American Association for the Advancement of Science. Paper 3, December 1964. A Steepest Ascent Trajectory Optimization Method which Reduces Memory Requirements. Computing Methods in Optimization Problems.

AIAA Progress in Astronautics and Aeronautics: Celestial Mechanics and Astrodynamics, edited by Saebehely, V. Optimisation of Multiple-Impulse Orbital Tetanus toxoid by the Maximum Principle. Academic Press Inc, New York, 1964.

Preliminary Investigations Relative to Multiple Rendezvous Between Circular Orbits. Tetanus toxoid Corp Report TDR 269 (4130-10)-4, 1964. Method of Characteristic Constants and Retro-Thrust Optimality in a Gravitational FieldNecessary and Sufficient Conditions. Diprophos Doubly Singular Problem in Optimal Interplanetary Guidance.

Minimum Impulse Coplanar Circle-ellipse Transfer. Rendezvous zu einem in elliptischer Bahn umlaufenden Ziel. Minimalprobleme der Luft-und Tetanus toxoid.

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