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 | ||
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Lo trovi qui: Univ. Federico II | ||
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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 | ||
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Lo trovi qui: Univ. Federico II | ||
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A comparison of a class of Earth-Moon orbits with a class of rotating Kepler orbits / / by R.F. Hoelker and B.P. Winston |
Autore | Hoelker R. F. <1912-> |
Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , November 1968 |
Descrizione fisica | 1 online resource (63 pages) : illustrations |
Collana | NASA/TN |
Soggetto topico |
Earth-Moon trajectories
Kepler laws Planets - Orbits Artificial satellites - Orbits Kepler's laws |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910715928603321 |
Hoelker R. F. <1912->
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Washington, D.C. : , : National Aeronautics and Space Administration, , November 1968 | ||
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Lo trovi qui: Univ. Federico II | ||
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Comparison of Space Shuttle Orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests / / Delma C. Freeman, Jr., and Barnard Spencer, Jr |
Autore | Freeman Delma C. |
Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 |
Descrizione fisica | 1 online resource (33 pages) : illustrations |
Collana | NASA technical paper |
Soggetto topico |
Ailerons
Approach and landing tests (STS) Elevons Lateral stability Longitudinal stability Space Shuttle orbiters Artificial satellites - Orbits Space vehicles - Landing Stability of space vehicles Wind tunnels - Ground simulators |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910707439503321 |
Freeman Delma C.
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[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 | ||
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Lo trovi qui: Univ. Federico II | ||
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Effects of cloud cover on selection of recovery sites for future earth orbital missions / / by Paul F. Holloway |
Autore | Holloway Paul F. |
Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , April 1969 |
Descrizione fisica | 1 online resource (19 pages) : illustrations, maps |
Collana | NASA technical note |
Soggetto topico |
Artificial satellites - Orbits
Cloud physics Cloud cover |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910713911603321 |
Holloway Paul F.
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Washington, D.C. : , : National Aeronautics and Space Administration, , April 1969 | ||
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Lo trovi qui: Univ. Federico II | ||
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Gravity model comparison using GEOS I long-arc orbital solutions / / by Francis J. Learch, James G. Marsh, and Brian O'Neill |
Autore | Lerch F. J (Francis J.) |
Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , June 1969 |
Descrizione fisica | 1 online resource (various pagings) : illustrations |
Collana | NASA technical note |
Soggetto topico |
Geodetic satellites
Gravitational fields - Mathematical models Artificial satellites - Orbits |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910713937203321 |
Lerch F. J (Francis J.)
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Washington, D.C. : , : National Aeronautics and Space Administration, , June 1969 | ||
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Lo trovi qui: Univ. Federico II | ||
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An introduction to orbit dynamics and its application to satellite-based earth monitoring missions [[electronic resource] /] / David R. Brooks |
Autore | Brooks David R |
Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , 1977 |
Descrizione fisica | 1 online resource (v, 80 pages) : illustrations |
Collana | NASA reference publication |
Soggetto topico |
Artificial satellites - Orbits
Remote sensing Earth resources technology satellites Earth surface Orbit calculation Satellite-borne instruments |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910701928903321 |
Brooks David R
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[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , 1977 | ||
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Lo trovi qui: Univ. Federico II | ||
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Nimbus II flight evaluation and engineering report, launch through orbit 5275 / / by Joseph J. McNaney and Bennie A. Palmer, Ralph Shapiro |
Autore | McNaney Joseph J. |
Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , February 1969 |
Descrizione fisica | 1 online resource (viii, 188 pages) : illustrations |
Collana | NASA/TN |
Soggetto topico |
Artificial satellites
Nimbus satellites Artificial satellites - Orbits |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910716026803321 |
McNaney Joseph J.
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Washington, D.C. : , : National Aeronautics and Space Administration, , February 1969 | ||
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Lo trovi qui: Univ. Federico II | ||
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Orbital mechanics [[electronic resource] /] / edited by Vladimir A. Chobotov |
Edizione | [3rd ed.] |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2002 |
Descrizione fisica | 1 online resource (450 p.) |
Disciplina | 629.4/113 |
Altri autori (Persone) | ChobotovVladimir A |
Collana | AIAA education series |
Soggetto topico |
Orbital mechanics
Artificial satellites - Orbits Navigation (Astronautics) |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-097-4
1-60119-208-8 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Preface""; ""About the Authors""; ""Table of Contents""; ""Chapter 1. Basic Concepts""; ""1.1 A Historical Perspective""; ""1.2 Velocity and Acceleration""; ""Problems""; ""Selected Solutions""; ""Chapter 2. Celestial Relationships""; ""2.1 Coordinate Systems""; ""2.2 Time Systems""; ""References""; ""Chapter 3. Keplerian Orbits""; ""3.1 Newton's Universal Law of Gravitation""; ""3.2 General and Restricted Two-Body Problem""; ""3.3 Conservation of Mechanical Energy""; ""3.4 Conservation of Angular Momentum""
""3.5 Orbital Parameters of a Satellite""""3.6 Orbital Elements""; ""References""; ""Problems""; ""Selected Solutions""; ""Chapter 4. Position and Velocity as a Function of Time""; ""4.1 General Relationships""; ""4.2 Solving Kepler's Equation""; ""4.3 A Universal Approach""; ""4.4 Expressions with f and g""; ""4.5 Summary of the Universal Approach""; ""4.6 The Classical Element Set""; ""4.7 The Rectangular Coordinate System""; ""4.8 Modified Classical to Cartesian Transformation""; ""4.9 Rectangular to Modified Classical Elements Transformation"" ""4.10 The Spherical (ADBARV) Coordinate System""""4.11 Rectangular to Spherical Transformation""; ""4.12 Spherical to Rectangular Transformation""; ""4.13 The Earth-Relative Spherical (LDBARV) Coordinate System""; ""4.14 Geodetic and Geocentric Altitudes""; ""4.15 Converting from Perigee/Apogee Radii to Perigee/Apogee Altitudes""; ""4.16 Converting from Perigee/Apogee Altitudes to Perigee/Apogee Radii""; ""References""; ""Problems""; ""Selected Solutions""; ""Chapter 5. Orbital Maneuvers""; ""5.1 Orbital Energy""; ""5.2 Single-Impulse Maneuvers"" ""5.3 Single- and Two-Impulse Transfer Comparison for Coplanar Transfers Between Elliptic Orbits That Differ Only in Their Apsidal Orientation""""5.4 Hohmann Transfer""; ""5.5 The Bi-elliptic Transfer""; ""5.6 Restricted Three-Impulse Plane Change Maneuver for Circular Orbits""; ""5.7 General Three-Impulse Plane Change Maneuver for Circular Orbit""; ""5.8 Hohmann Transfer with Split-Plane Change""; ""5.9 Bi-elliptic Transfer with Split-Plane Change""; ""5.10 Transfer Between Coplanar Elliptic Orbits""; ""References""; ""Problems""; ""Selected Solutions"" ""Chapter 6. Complications to Impulsive Maneuvers""""6.1 N-Impulse Maneuvers""; ""6.2 Fixed-Impulse Transfers""; ""6.3 Finite-Duration Burns: Gravity Losses""; ""6.4 Very Low Thrust Transfers""; ""References""; ""Problems""; ""Selected Solutions""; ""Chapter 7. Relative Motion in Orbit""; ""7.1 Space Rendezvous""; ""7.2 Terminal Rendezvous""; ""7.3 Applications of Rendezvous Equations""; ""7.4 An Exact Analytical Solution for Two-Dimensional Relative Motion""; ""7.5 Optimal Multiple-Impulse Rendezvous""; ""References""; ""Problems""; ""Selected Solutions"" ""Chapter 8. Introduction to Orbit Perturbations"" |
Record Nr. | UNINA-9910451099403321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2002 | ||
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Lo trovi qui: Univ. Federico II | ||
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Orbital mechanics [[electronic resource] /] / edited by Vladimir A. Chobotov |
Edizione | [3rd ed.] |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2002 |
Descrizione fisica | 1 online resource (450 p.) |
Disciplina | 629.4/113 |
Altri autori (Persone) | ChobotovVladimir A |
Collana | AIAA education series |
Soggetto topico |
Orbital mechanics
Artificial satellites - Orbits Navigation (Astronautics) |
ISBN |
1-60086-097-4
1-60119-208-8 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Preface""; ""About the Authors""; ""Table of Contents""; ""Chapter 1. Basic Concepts""; ""1.1 A Historical Perspective""; ""1.2 Velocity and Acceleration""; ""Problems""; ""Selected Solutions""; ""Chapter 2. Celestial Relationships""; ""2.1 Coordinate Systems""; ""2.2 Time Systems""; ""References""; ""Chapter 3. Keplerian Orbits""; ""3.1 Newton's Universal Law of Gravitation""; ""3.2 General and Restricted Two-Body Problem""; ""3.3 Conservation of Mechanical Energy""; ""3.4 Conservation of Angular Momentum""
""3.5 Orbital Parameters of a Satellite""""3.6 Orbital Elements""; ""References""; ""Problems""; ""Selected Solutions""; ""Chapter 4. Position and Velocity as a Function of Time""; ""4.1 General Relationships""; ""4.2 Solving Kepler's Equation""; ""4.3 A Universal Approach""; ""4.4 Expressions with f and g""; ""4.5 Summary of the Universal Approach""; ""4.6 The Classical Element Set""; ""4.7 The Rectangular Coordinate System""; ""4.8 Modified Classical to Cartesian Transformation""; ""4.9 Rectangular to Modified Classical Elements Transformation"" ""4.10 The Spherical (ADBARV) Coordinate System""""4.11 Rectangular to Spherical Transformation""; ""4.12 Spherical to Rectangular Transformation""; ""4.13 The Earth-Relative Spherical (LDBARV) Coordinate System""; ""4.14 Geodetic and Geocentric Altitudes""; ""4.15 Converting from Perigee/Apogee Radii to Perigee/Apogee Altitudes""; ""4.16 Converting from Perigee/Apogee Altitudes to Perigee/Apogee Radii""; ""References""; ""Problems""; ""Selected Solutions""; ""Chapter 5. Orbital Maneuvers""; ""5.1 Orbital Energy""; ""5.2 Single-Impulse Maneuvers"" ""5.3 Single- and Two-Impulse Transfer Comparison for Coplanar Transfers Between Elliptic Orbits That Differ Only in Their Apsidal Orientation""""5.4 Hohmann Transfer""; ""5.5 The Bi-elliptic Transfer""; ""5.6 Restricted Three-Impulse Plane Change Maneuver for Circular Orbits""; ""5.7 General Three-Impulse Plane Change Maneuver for Circular Orbit""; ""5.8 Hohmann Transfer with Split-Plane Change""; ""5.9 Bi-elliptic Transfer with Split-Plane Change""; ""5.10 Transfer Between Coplanar Elliptic Orbits""; ""References""; ""Problems""; ""Selected Solutions"" ""Chapter 6. Complications to Impulsive Maneuvers""""6.1 N-Impulse Maneuvers""; ""6.2 Fixed-Impulse Transfers""; ""6.3 Finite-Duration Burns: Gravity Losses""; ""6.4 Very Low Thrust Transfers""; ""References""; ""Problems""; ""Selected Solutions""; ""Chapter 7. Relative Motion in Orbit""; ""7.1 Space Rendezvous""; ""7.2 Terminal Rendezvous""; ""7.3 Applications of Rendezvous Equations""; ""7.4 An Exact Analytical Solution for Two-Dimensional Relative Motion""; ""7.5 Optimal Multiple-Impulse Rendezvous""; ""References""; ""Problems""; ""Selected Solutions"" ""Chapter 8. Introduction to Orbit Perturbations"" |
Record Nr. | UNINA-9910783937203321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2002 | ||
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Lo trovi qui: Univ. Federico II | ||
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