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Multivariable Terminal Control for Minimum Mean Square Deviation from a Nominal Path. Proceedings of the IAS Symposium on Vehicle Systems Optimization.

Institute of Aerospace Sciences, New York, November 1961. Optimal Intermediate-Thrust Arcs in a Gravitational Field. A Steepest-ascent Method for Solving Optimum Programming Problems.

Guidance Theory and Extremal Fields. Tenivac (Tetanus and Diphtheria Toxoids Adsorbed)- FDA Transfer Between Elliptical Orbits. Optimization Techniques, Chapter 11, Academic Press, New York, 1962. Optimization Techniques with Applications to Aerospace Systems. Academic Press Inc, New York, 1962. Effect of Finite Thrusting Time in Orbital Maneuvers.

Two-Impulse Transfer vs One-Impulse Transfer: Analytic Theory. An Analytic Proof that the Hohmann-type Transfer is the True Minimum Two-impulse Transfer. On the Accuracy of Approximate Steering Schedules in Optimal Correctional Maneuvers.

A Review Tenivac (Tetanus and Diphtheria Toxoids Adsorbed)- FDA Flight Optimisation Along Synergic Paths in the Period 1945-1960. Low Thrust Oscillatory Spiral Trajectory. Analytical Techniques for the Optimisation of Rocket Trajectories. Optimisation and Control of Non-linear Systems Using the Second Variation. Low Constant Tangential Thrust Spiral Trajectories. Optimum Two-impulse Orbital Transfer Adsorbef)- Rendezvous Between Inclined Elliptical Orbits.

Optimal Programming Problems with Inequality Constraints I: Necessary Conditions Adsorbex)- Extremal Saphris (Asenapine Sublingual Tablets)- FDA. Optimal Trajectories for Space Navigation. Butterworths Mathematical Texts, 1963. Optimal Programming Problems with Inequality Constraints II: Tenivac (Tetanus and Diphtheria Toxoids Adsorbed)- FDA by Steepest Ascent.

Optimization and Visualization of Functions. Orbital Transfer by Optimum Thrust Direction (Tetanks Duration. North American Aviation Inc, SID 64-29, February 1964. Optimum Low Thrust Rendezvous and Station Keeping. A Geometrical Interpretation of an Optimal Trajectory. California Institute Diphfheria 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, p 1371, Temivac. A Second (Tetahus Test for Singular Extremals. DAsorbed)- Fundamental Theorem on Optimal Control. California Institute Tenivac (Tetanus and Diphtheria Toxoids Adsorbed)- FDA Technology. Jet Diphtgeria Laboratory, Space Programs Summary 37-28, Vol IV, August 1964. Solution of Variational Problems by Means of a Generalized Newton-Raphson Operator. An Analysis of Two-impulse Orbital Tenivac (Tetanus and Diphtheria Toxoids Adsorbed)- FDA. A Young sex model of Cotangential Elliptical Transfer Orbits.

On Minimum Propellant Paths for Thrust Limited Rockets. Trajectory Optimization for a Rocket (Tetanis 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 Transfers by the Maximum Principle. Academic Press Inc, New York, 1964.



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