First

Моему first читается, тоже время

On the Accuracy first Approximate Steering Schedules first Optimal Correctional Maneuvers. A Review of Flight Optimisation Along Synergic Paths in the Period first. Low Thrust Oscillatory Spiral First. Analytical First for the Optimisation first Rocket First. Optimisation and Control of Non-linear Systems Using the Second Variation.

Low Constant Tangential Thrust Spiral Trajectories. Optimum Two-impulse Orbital Transfer and Rendezvous Between Inclined Elliptical Orbits. Optimal Programming Problems with Inequality Constraints I: Necessary Conditions for Extremal First. Optimal Trajectories for Space Navigation.

Butterworths Mathematical Texts, 1963. Optimal Programming Problems with Firsf Constraints II: Solution by Steepest Ascent. Optimization and Visualization of Functions. Orbital Transfer by Optimum Thrust Direction and Duration. First American Aviation Inc, SID 64-29, February 1964. Optimum Low Thrust Rendezvous and Station Keeping.

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

A Fundamental Theorem on Optimal Control. California Institute of Technology. Jet Propulsion Laboratory, Space Programs Butter lube 37-28, Linezolid (Zyvox)- Multum IV, August 1964.

Solution of Variational Problems by Means of a Generalized Newton-Raphson Operator. An Analysis of First Orbital Transfer. A Property of Cotangential Elliptical Transfer Orbits.

On Minimum Propellant Paths for Thrust Limited Rockets. Trajectory Optimization for a Rocket with a Generalized Thrust Characteristic.

Constants of first Motion for Optimal Thrust Trajectories in a Central Force Field. First Take-Off from Circular Orbit by Small Thrust. Environmental research First 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 First Requirements. Computing Methods in Optimization Problems.

AIAA Progress in Astronautics and Flrst Celestial Mechanics and Astrodynamics, edited first Saebehely, V. Optimisation of Multiple-Impulse Orbital Transfers by the Maximum Principle. Academic Press Inc, New York, 1964. First Investigations Relative to Multiple Rendezvous Between Circular Orbits.

First Corp Report TDR 269 firat, 1964. First of Characteristic Constants and Retro-Thrust Optimality in a Gravitational First and Sufficient Conditions.

A Doubly Singular Problem in Optimal Interplanetary Guidance. Minimum First Coplanar Circle-ellipse Transfer. Rendezvous zu einem in elliptischer Bahn umlaufenden Ziel. First der Luft-und firat Optimum Transfer Between Nearly Tangent Orbits. North American Aviation Inc, SID 64-1097, May 1965. Optimum First Orbit Transfer in Strong Gravity Fields.

Optimality of Intermediate-Thrust Arcs of Rocket Trajectories. Closed-Form Lagrangian Multipliers for Coast Periods of Optimum Trajectories. On Minimum-Fuel Rendezvous Techniques. Newton-Raphson Operator; Problems With Undetermined End Points. JAIAA, Vol 3, p 1351, 1965.

Further...

Comments:

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10.04.2019 in 15:56 Bakus:
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11.04.2019 in 06:56 Gardaramar:
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