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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
A comparison of a class of Earth-Moon orbits with a class of rotating Kepler orbits / / by R.F. Hoelker and B.P. Winston
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->  
Washington, D.C. : , : National Aeronautics and Space Administration, , November 1968
Materiale a stampa
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
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.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980
Materiale a stampa
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
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.  
Washington, D.C. : , : National Aeronautics and Space Administration, , April 1969
Materiale a stampa
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
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.)  
Washington, D.C. : , : National Aeronautics and Space Administration, , June 1969
Materiale a stampa
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
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  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , 1977
Materiale a stampa
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
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.  
Washington, D.C. : , : National Aeronautics and Space Administration, , February 1969
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Orbital mechanics [[electronic resource] /] / edited by Vladimir A. Chobotov
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
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

Data di pubblicazione