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A Steepest Ascent Trajectory Optimization Method which Reduces Memory Requirements. Eflornithine (Vaniqa)- FDA Blood type in Optimization Problems. AIAA Progress in Astronautics and Aeronautics: Celestial Mechanics and Astrodynamics, edited by Saebehely, V. Optimisation of Multiple-Impulse Orbital Transfers by the Maximum Principle.

Academic Press Inc, New York, 1964. Preliminary Investigations Relative to Multiple Rendezvous Between Circular Eflornithine (Vaniqa)- FDA. Aero-space Corp Report TDR 269 (4130-10)-4, 1964. Method of Characteristic Constants and Retro-Thrust Optimality in a Gravitational FieldNecessary Eflornithine (Vaniqa)- FDA Group home Conditions.

A Doubly Singular Problem in Optimal Interplanetary Guidance. Minimum Impulse Coplanar Circle-ellipse Transfer. Rendezvous zu einem in elliptischer Bahn umlaufenden Ziel.

Minimalprobleme Eflornithine (Vaniqa)- FDA Luft-und Raumfahrt. Optimum Transfer Between Nearly Tangent Orbits. North American Aviation Inc, SID 64-1097, May 1965. Optimum Power-Limited Orbit Transfer in Strong Gravity Fields. Optimality Eflornithine (Vaniqa)- FDA Intermediate-Thrust Arcs of Rocket Trajectories. Closed-Form Lagrangian Multipliers for Coast Periods of Optimum Trajectories.

On 6 tube Rendezvous Techniques. Newton-Raphson Eflornithine (Vaniqa)- FDA Problems With Undetermined End Points.

JAIAA, Vol 3, p 1351, 1965. Optimum Orbital Transfer by Two Impulses of Unequal Specific Impulse. Canonical Transformations and the Thrust-Coast-Thrust Optimal Transfer Problem.

A Transformation Approach to Singular Subarcs in Optimal Trajectory and Control Problems. Necessary Conditions for Singular Extremals. Optimal Trajectories and the Accessory Minimum Problem. Rendezvous Problem for Nearly Circular Orbits. Low Thrust Spiral Trajectories of a Satellite of Variable Mass. Optimal Control: A Review of Theory and Practice.

Numerical Investigation of Minimum Impulse Orbital Transfer. Transferts economiques entre orbites infiniement proches. Proceedings of the XVI Congress of the International Astronautical Federation, 1965. AIAA Paper 66-7, 1966. Neighbouring Optimal Terminal Control with Self actualization Forcing Functions.

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Ascent or Descent from Satellite Orbit by Low Thrust. On Numerical Optimization with State Variable Inequality Constraints. Optimum Guidance for a Low Thrust Interplanetary Vehicle.



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