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Celestial mechanics and astrodynamics [[electronic resource] /] / edited by Victor G. Szebehely
Celestial mechanics and astrodynamics [[electronic resource] /] / edited by Victor G. Szebehely
Pubbl/distr/stampa New York, : Academic Press, 1964
Descrizione fisica 1 online resource (765 p.)
Disciplina 521.1
Altri autori (Persone) SzebehelyVictor G. <1921->
Collana Progress in astronautics and aeronautics
Soggetto topico Astronautics
Artificial satellites - Orbits
Soggetto genere / forma Electronic books.
ISBN 1-60086-488-0
1-60086-269-1
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto ""Cover""; ""Title""; ""Copyright""; ""The ARS Astrodynamics Committee 1962""; ""The AIAA Astrodynamics Committee 1963""; ""The Astrodynamics Conference Committee 1963""; ""Preface""; ""Astrodynamics in the AIAA""; ""Contents""; ""I. Orbit Prediction and General Perturbations""; ""Numerical Aspects of Uniformly Valid Asymptotic Approximations for a Class of Trajectories in the Restricted Three-Body Problem""; ""A Group of Earth-to-Moon Trajectories with Consecutive Collisions""; ""Two Fixed Center Approximations to the Restricted Problem""
""A High-Order Perturbation Theory Using Rectangular Coordinates""""Trajectories of Satellites under the Influence of Air Drag""; ""II. Astronomical Constants and Physical Properties""; ""System of Astronomical Constants""; ""The Evaluation of Certain Astronomical Constants from the Radio Tracking of Mariner II""; ""Atmospheric Density Determination from Satellite Observations""; ""III. Orbit Selection""; ""Probabilistic Evaluation of Satellite Missions Involving Ground Coverage""; ""Orbital Aspects of Nonsynchronous Communication Satellite Systems""
""Guidance of Unmanned Lunar and Interplanetary Spacecraft""""An Approximate Method for Computing Error Coefficient Matrices for Lunar Trajectories""; ""Minimum Lunar Orbit Inclination to Lunar Equatorial Plane for Earth-Launched Vehicle""; ""General Characteristics of the Launch Window for Orbital Launch to the Moon""; ""Launch Windows for Highly Eccentric Orbits""; ""Moon-to-Earth Trajectories""; ""An Analysis of Free Return Circumlunar Trajectories""; ""Free Return Circumlunar Trajectories from Launch Windows with Fixed Launch Azimuths""
""IV. Orbit Mechanics of the Ranger and Mariner Missions""""Trajectory Design for Ranger and Mariner Missions""; ""Boost Vehicle Trajectories for Ranger and Mariner Programs""; ""Launch-to-Mission Completion Targeting for Ranger and Mariner Missions""; ""V. Orbit Transfer and Trajectory Optimization""; ""A Trajectory Optimization Technique Based upon the Theory of the Second Variation""; ""Minimum Impulse Transfer""; ""On Some Single-Impulse Transfer Problems""; ""Analysis of the Orbital Transfer Problem in Three-Dimensional Space""; ""VI. Orbit Determination""
""Position and Velocity Estimates by Trajectory Rectification""""Self-Contained Orbit Determination Techniques""; ""Linearized Drag Analysis and Orbit Determination""; ""Orbit Determination in the Presence of Systematic Errors""; ""Contributors to Volume 14""
Record Nr. UNINA-9910457249903321
New York, : Academic Press, 1964
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Celestial mechanics and astrodynamics [[electronic resource] /] / edited by Victor G. Szebehely
Celestial mechanics and astrodynamics [[electronic resource] /] / edited by Victor G. Szebehely
Pubbl/distr/stampa New York, : Academic Press, 1964
Descrizione fisica 1 online resource (765 p.)
Disciplina 521.1
Altri autori (Persone) SzebehelyVictor G. <1921->
Collana Progress in astronautics and aeronautics
Soggetto topico Astronautics
Artificial satellites - Orbits
ISBN 1-60086-488-0
1-60086-269-1
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto ""Cover""; ""Title""; ""Copyright""; ""The ARS Astrodynamics Committee 1962""; ""The AIAA Astrodynamics Committee 1963""; ""The Astrodynamics Conference Committee 1963""; ""Preface""; ""Astrodynamics in the AIAA""; ""Contents""; ""I. Orbit Prediction and General Perturbations""; ""Numerical Aspects of Uniformly Valid Asymptotic Approximations for a Class of Trajectories in the Restricted Three-Body Problem""; ""A Group of Earth-to-Moon Trajectories with Consecutive Collisions""; ""Two Fixed Center Approximations to the Restricted Problem""
""A High-Order Perturbation Theory Using Rectangular Coordinates""""Trajectories of Satellites under the Influence of Air Drag""; ""II. Astronomical Constants and Physical Properties""; ""System of Astronomical Constants""; ""The Evaluation of Certain Astronomical Constants from the Radio Tracking of Mariner II""; ""Atmospheric Density Determination from Satellite Observations""; ""III. Orbit Selection""; ""Probabilistic Evaluation of Satellite Missions Involving Ground Coverage""; ""Orbital Aspects of Nonsynchronous Communication Satellite Systems""
""Guidance of Unmanned Lunar and Interplanetary Spacecraft""""An Approximate Method for Computing Error Coefficient Matrices for Lunar Trajectories""; ""Minimum Lunar Orbit Inclination to Lunar Equatorial Plane for Earth-Launched Vehicle""; ""General Characteristics of the Launch Window for Orbital Launch to the Moon""; ""Launch Windows for Highly Eccentric Orbits""; ""Moon-to-Earth Trajectories""; ""An Analysis of Free Return Circumlunar Trajectories""; ""Free Return Circumlunar Trajectories from Launch Windows with Fixed Launch Azimuths""
""IV. Orbit Mechanics of the Ranger and Mariner Missions""""Trajectory Design for Ranger and Mariner Missions""; ""Boost Vehicle Trajectories for Ranger and Mariner Programs""; ""Launch-to-Mission Completion Targeting for Ranger and Mariner Missions""; ""V. Orbit Transfer and Trajectory Optimization""; ""A Trajectory Optimization Technique Based upon the Theory of the Second Variation""; ""Minimum Impulse Transfer""; ""On Some Single-Impulse Transfer Problems""; ""Analysis of the Orbital Transfer Problem in Three-Dimensional Space""; ""VI. Orbit Determination""
""Position and Velocity Estimates by Trajectory Rectification""""Self-Contained Orbit Determination Techniques""; ""Linearized Drag Analysis and Orbit Determination""; ""Orbit Determination in the Presence of Systematic Errors""; ""Contributors to Volume 14""
Record Nr. UNINA-9910781417803321
New York, : Academic Press, 1964
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Celestial mechanics and astrodynamics [[electronic resource] /] / edited by Victor G. Szebehely
Celestial mechanics and astrodynamics [[electronic resource] /] / edited by Victor G. Szebehely
Pubbl/distr/stampa New York, : Academic Press, 1964
Descrizione fisica 1 online resource (765 p.)
Disciplina 521.1
Altri autori (Persone) SzebehelyVictor G. <1921->
Collana Progress in astronautics and aeronautics
Soggetto topico Astronautics
Artificial satellites - Orbits
ISBN 1-60086-488-0
1-60086-269-1
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto ""Cover""; ""Title""; ""Copyright""; ""The ARS Astrodynamics Committee 1962""; ""The AIAA Astrodynamics Committee 1963""; ""The Astrodynamics Conference Committee 1963""; ""Preface""; ""Astrodynamics in the AIAA""; ""Contents""; ""I. Orbit Prediction and General Perturbations""; ""Numerical Aspects of Uniformly Valid Asymptotic Approximations for a Class of Trajectories in the Restricted Three-Body Problem""; ""A Group of Earth-to-Moon Trajectories with Consecutive Collisions""; ""Two Fixed Center Approximations to the Restricted Problem""
""A High-Order Perturbation Theory Using Rectangular Coordinates""""Trajectories of Satellites under the Influence of Air Drag""; ""II. Astronomical Constants and Physical Properties""; ""System of Astronomical Constants""; ""The Evaluation of Certain Astronomical Constants from the Radio Tracking of Mariner II""; ""Atmospheric Density Determination from Satellite Observations""; ""III. Orbit Selection""; ""Probabilistic Evaluation of Satellite Missions Involving Ground Coverage""; ""Orbital Aspects of Nonsynchronous Communication Satellite Systems""
""Guidance of Unmanned Lunar and Interplanetary Spacecraft""""An Approximate Method for Computing Error Coefficient Matrices for Lunar Trajectories""; ""Minimum Lunar Orbit Inclination to Lunar Equatorial Plane for Earth-Launched Vehicle""; ""General Characteristics of the Launch Window for Orbital Launch to the Moon""; ""Launch Windows for Highly Eccentric Orbits""; ""Moon-to-Earth Trajectories""; ""An Analysis of Free Return Circumlunar Trajectories""; ""Free Return Circumlunar Trajectories from Launch Windows with Fixed Launch Azimuths""
""IV. Orbit Mechanics of the Ranger and Mariner Missions""""Trajectory Design for Ranger and Mariner Missions""; ""Boost Vehicle Trajectories for Ranger and Mariner Programs""; ""Launch-to-Mission Completion Targeting for Ranger and Mariner Missions""; ""V. Orbit Transfer and Trajectory Optimization""; ""A Trajectory Optimization Technique Based upon the Theory of the Second Variation""; ""Minimum Impulse Transfer""; ""On Some Single-Impulse Transfer Problems""; ""Analysis of the Orbital Transfer Problem in Three-Dimensional Space""; ""VI. Orbit Determination""
""Position and Velocity Estimates by Trajectory Rectification""""Self-Contained Orbit Determination Techniques""; ""Linearized Drag Analysis and Orbit Determination""; ""Orbit Determination in the Presence of Systematic Errors""; ""Contributors to Volume 14""
Record Nr. UNINA-9910811691803321
New York, : Academic Press, 1964
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Methods in astrodynamics and celestial mechanics [[electronic resource] /] / edited by Raynor L. Duncombe, Victor G. Szebehely
Methods in astrodynamics and celestial mechanics [[electronic resource] /] / edited by Raynor L. Duncombe, Victor G. Szebehely
Pubbl/distr/stampa New York, : Academic Press, 1966
Descrizione fisica 1 online resource (453 p.)
Disciplina 629.4ll
Altri autori (Persone) DuncombeRaynor L
SzebehelyVictor G. <1921->
Collana Progress in astronautics and aeronautics
Soggetto topico Astrodynamics
Soggetto genere / forma Electronic books.
ISBN 1-60086-491-0
1-60086-272-1
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto ""Cover""; ""Title""; ""Copyright""; ""The AIAA Astrodynamics Committee 1965""; ""The Astrodynamics Specialist Conference Committee 1965""; ""Preface""; ""Contents""; ""I. Behavior of Bodies near Libration Points""; ""Theory and Application of Motion around Equilibrium Positions""; ""Limiting Orbits at the Equilateral Centers of Libration""; ""Motion in the Vicinity of Libration Points of a Generalized Restricted Three-Body Model""; ""Resonances Affecting Motion near the Earth-Moon Equilateral Libration Points""; ""Effect of Initial Configurations on Libration Point Motion""
""Analytical Determination of Characteristic Exponents""""II. Asymptotic Representations of Space Vehicle Trajectories""; ""Generalized Method of Averaging and the von Zeipel Method""; ""Take-off from a Circular Orbit by a Small Thrust""; ""Matched Asymptotic Expansions, Patched Conics, and the Computation of Interplanetary Trajectories""; ""A Uniformly Valid Asymptotic Representation of Satellite Motion around the Smaller Primary in the Restricted Three-Body Problem""; ""Asymptotic Representations for Solutions to the Differential Equations of Satellite Theory""
""III. Orbit Determination and Mission Analysis""""Error Equations of Inertial Navigation with Special Application to Orbital Determination and Guidance""; ""Efficient and Accurate Orbit Prediction for Very Long Periods of Time""; ""Parameter Hunting Procedures""; ""Accuracy in the Determination of Lunar Transponder Location from Postarrival Tracking""; ""Interplanetary Maneuvers in Manned Helionautical Missions""; ""IV. Optimization in Astrodynamics""; ""A General Method for Selection and Optimization of Trajectories""
""Application of a Finite-Difference Newton-Raphson Algorithm to Problems of Low-Thrust Trajectory Optimization""""Nonlinear Optimal Control Problems with Control Appearing Linearly""; ""Contributors To Volume 17""
Record Nr. UNINA-9910457212303321
New York, : Academic Press, 1966
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Methods in astrodynamics and celestial mechanics [[electronic resource] /] / edited by Raynor L. Duncombe, Victor G. Szebehely
Methods in astrodynamics and celestial mechanics [[electronic resource] /] / edited by Raynor L. Duncombe, Victor G. Szebehely
Pubbl/distr/stampa New York, : Academic Press, 1966
Descrizione fisica 1 online resource (453 p.)
Disciplina 629.4ll
Altri autori (Persone) DuncombeRaynor L
SzebehelyVictor G. <1921->
Collana Progress in astronautics and aeronautics
Soggetto topico Astrodynamics
ISBN 1-60086-491-0
1-60086-272-1
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto ""Cover""; ""Title""; ""Copyright""; ""The AIAA Astrodynamics Committee 1965""; ""The Astrodynamics Specialist Conference Committee 1965""; ""Preface""; ""Contents""; ""I. Behavior of Bodies near Libration Points""; ""Theory and Application of Motion around Equilibrium Positions""; ""Limiting Orbits at the Equilateral Centers of Libration""; ""Motion in the Vicinity of Libration Points of a Generalized Restricted Three-Body Model""; ""Resonances Affecting Motion near the Earth-Moon Equilateral Libration Points""; ""Effect of Initial Configurations on Libration Point Motion""
""Analytical Determination of Characteristic Exponents""""II. Asymptotic Representations of Space Vehicle Trajectories""; ""Generalized Method of Averaging and the von Zeipel Method""; ""Take-off from a Circular Orbit by a Small Thrust""; ""Matched Asymptotic Expansions, Patched Conics, and the Computation of Interplanetary Trajectories""; ""A Uniformly Valid Asymptotic Representation of Satellite Motion around the Smaller Primary in the Restricted Three-Body Problem""; ""Asymptotic Representations for Solutions to the Differential Equations of Satellite Theory""
""III. Orbit Determination and Mission Analysis""""Error Equations of Inertial Navigation with Special Application to Orbital Determination and Guidance""; ""Efficient and Accurate Orbit Prediction for Very Long Periods of Time""; ""Parameter Hunting Procedures""; ""Accuracy in the Determination of Lunar Transponder Location from Postarrival Tracking""; ""Interplanetary Maneuvers in Manned Helionautical Missions""; ""IV. Optimization in Astrodynamics""; ""A General Method for Selection and Optimization of Trajectories""
""Application of a Finite-Difference Newton-Raphson Algorithm to Problems of Low-Thrust Trajectory Optimization""""Nonlinear Optimal Control Problems with Control Appearing Linearly""; ""Contributors To Volume 17""
Record Nr. UNINA-9910781403803321
New York, : Academic Press, 1966
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Methods in astrodynamics and celestial mechanics [[electronic resource] /] / edited by Raynor L. Duncombe, Victor G. Szebehely
Methods in astrodynamics and celestial mechanics [[electronic resource] /] / edited by Raynor L. Duncombe, Victor G. Szebehely
Pubbl/distr/stampa New York, : Academic Press, 1966
Descrizione fisica 1 online resource (453 p.)
Disciplina 629.4ll
Altri autori (Persone) DuncombeRaynor L
SzebehelyVictor G. <1921->
Collana Progress in astronautics and aeronautics
Soggetto topico Astrodynamics
ISBN 1-60086-491-0
1-60086-272-1
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto ""Cover""; ""Title""; ""Copyright""; ""The AIAA Astrodynamics Committee 1965""; ""The Astrodynamics Specialist Conference Committee 1965""; ""Preface""; ""Contents""; ""I. Behavior of Bodies near Libration Points""; ""Theory and Application of Motion around Equilibrium Positions""; ""Limiting Orbits at the Equilateral Centers of Libration""; ""Motion in the Vicinity of Libration Points of a Generalized Restricted Three-Body Model""; ""Resonances Affecting Motion near the Earth-Moon Equilateral Libration Points""; ""Effect of Initial Configurations on Libration Point Motion""
""Analytical Determination of Characteristic Exponents""""II. Asymptotic Representations of Space Vehicle Trajectories""; ""Generalized Method of Averaging and the von Zeipel Method""; ""Take-off from a Circular Orbit by a Small Thrust""; ""Matched Asymptotic Expansions, Patched Conics, and the Computation of Interplanetary Trajectories""; ""A Uniformly Valid Asymptotic Representation of Satellite Motion around the Smaller Primary in the Restricted Three-Body Problem""; ""Asymptotic Representations for Solutions to the Differential Equations of Satellite Theory""
""III. Orbit Determination and Mission Analysis""""Error Equations of Inertial Navigation with Special Application to Orbital Determination and Guidance""; ""Efficient and Accurate Orbit Prediction for Very Long Periods of Time""; ""Parameter Hunting Procedures""; ""Accuracy in the Determination of Lunar Transponder Location from Postarrival Tracking""; ""Interplanetary Maneuvers in Manned Helionautical Missions""; ""IV. Optimization in Astrodynamics""; ""A General Method for Selection and Optimization of Trajectories""
""Application of a Finite-Difference Newton-Raphson Algorithm to Problems of Low-Thrust Trajectory Optimization""""Nonlinear Optimal Control Problems with Control Appearing Linearly""; ""Contributors To Volume 17""
Record Nr. UNINA-9910810028103321
New York, : Academic Press, 1966
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui