LANDSAT-5 orbit adjust maneuver report / / prepared by P.J. Hassett, R.L. Johnson |
Autore | Hassett P. J. |
Pubbl/distr/stampa | [Silver Spring, MD] : , : Computer Sciences Corporation, , June 1984 |
Descrizione fisica | 1 online resource (63 unnumbered pages) : illustrations |
Collana | NASA-CR |
Soggetto topico |
Landsat 5
Orbital maneuvers Orbital mechanics Satellite control Satellite ground tracks |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910703860103321 |
Hassett P. J. | ||
[Silver Spring, MD] : , : Computer Sciences Corporation, , June 1984 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Linear and regular celestial mechanics : perturbed two-body motion, numerical methods, canonical theory / E. L. Stiefel, G. Scheifele |
Autore | Stiefel, Eduard L. |
Pubbl/distr/stampa | Berlin : Springer-Verlag, 1971 |
Descrizione fisica | ix, 301 p. : ill. ; 24 cm. |
Disciplina | 521 |
Altri autori (Persone) | Scheifele, G. |
Collana | Grundlehren der mathematischen Wissenschaften = A series of comprehensive studies in mathematics, 0072-7830 ; 174 |
Soggetto topico |
Celestial mechanics
Hamilton-Jacobi equations Orbital mechanics Two-body problem |
ISBN | 3540051198 |
Classificazione |
AMS 70F05
AMS 70F15 AMS 70H15 AMS 70H20 AMS 70M20 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNISALENTO-991001085829707536 |
Stiefel, Eduard L. | ||
Berlin : Springer-Verlag, 1971 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. del Salento | ||
|
Orbital and celestial mechanics [[electronic resource] /] / John P. Vinti ; edited by Gim J. Der, Nino L. Bonavito |
Autore | Vinti John P (John Pascal), <1907-> |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1998 |
Descrizione fisica | 1 online resource (415 p.) |
Disciplina | 629.4/113 |
Altri autori (Persone) |
DerGim J
BonavitoNino L |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Orbital mechanics
Celestial mechanics Astrodynamics |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-648-4
1-60086-429-5 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Cover; Title; Copyright; Foreword; Table of Contents; Preface; Introduction; Chapter 1 Newton's Laws; I. Newton's Laws of Motion; II. Newton's Law of Gravitation; III. The Gravitational Potential; IV. Gravitational Flux and Gauss' Theorem; V. Gravitational Properties of a True Sphere; Chapter 2 The Two-Body Problem; I. Reduction to the One-Center Problem; II. The One-Center Problem; III. The Laplace Vector; IV. The Conic Section Solutions; V. Elliptic Orbits; VI. Spherical Trigonometry; VII. Orbit in Space; VIII. Orbit Determination from Initial Values; Chapter 3 Lagrangian Dynamics
I. VariationsII. D'Alembert's Principle; III. Hamilton's Principle; IV. Lagrange's Equations; Reference; Chapter 4 The Hamiltonian Equations; I. An Important Theorem; II. Ignorable Variables; Chapter 5 Canonical Transformations; I. The Condition of Exact Differentials; II. Canonical Generating Functions; III. Extended Point Transformation; IV. Transformation from Plane Rectangular to Plane Polar Coordinates; V. The Jacobi Integral; References; Chapter 6 Hamilton-Jacobi Theory; I. The Hamilton-Jacobi Equation; II. An Important Special Case III. The Hamilton-Jacobi Equation for the Kepler ProblemIV. The Integrals for the Kepler Problem; V. Relations Connecting β[sub(2)] and β[sub(3)] with ω and Ω; VI. Summary; Bibliography; Chapter 7 Hamilton-Jacobi Perturbation Theory; Bibliography; Chapter 8 The Vinti Spheroidal Method for Satellite Orbits and Ballistic Trajectories; I. Introduction; II. The Coordinates and the Hamiltonian; III. The Hamilton-Jacobi Equation; IV. Laplace's Equation; V. Expansion of Potential in Spherical Harmonics; VI. Return to the HJ Equation; VII. The Kinematic Equations; VIII. Orbital Elements IX. Factoring the QuarticsX. The ρ Integrals; XI. The η Integrals; XII. The Mean Frequencies; XIII. Assembly of the Kinematic Equations; XIV. Solution of the Kinematic Equations; XV. The Periodic Terms; XVI. The Right Ascension Φ; XVII. Further Developments; References; Chapter 9 Delaunay Variables; Reference; Chapter 10 The Lagrange Planetary Equations; I. Semi-Major Axis; II. Eccentricity; III. Inclination; IV. Mean Anomaly; V. The Argument of Pericenter; VI. The Longitude of the Node; VII. Summary; Reference; Chapter 11 The Planetary Disturbing Function; Bibliography Chapter 12 Gaussian Variational Equations for the Jacobi ElementsReferences; Chapter 13 Gaussian Variational Equations for the Keplerian Elements; I. Preliminaries; II. Equations for α[sub(1)] and a; III. Equations for α[sub(2)] and e; IV. Equations for α[sub(3)] and I; V. Equations for β[sub(3)] = Ω; VI. Equations for β[sub(2)] = ω; VII. Equations for β[sub(1)] and l; VIII. Summary; Chapter 14 Potential Theory; I. Introduction; II. Laplace's Equation; III. The Eigenvalue Problem; IV. The R(r) Equation; V. The Assembled Solution; VI. Legendre Polynomials; VII. The Results for P[sub(n)](x) VIII. The 0 Solution for m > 0 |
Record Nr. | UNINA-9910457217703321 |
Vinti John P (John Pascal), <1907-> | ||
Reston, Va., : American Institute of Aeronautics and Astronautics, c1998 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Orbital and celestial mechanics [[electronic resource] /] / John P. Vinti ; edited by Gim J. Der, Nino L. Bonavito |
Autore | Vinti John P (John Pascal), <1907-> |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1998 |
Descrizione fisica | 1 online resource (415 p.) |
Disciplina | 629.4/113 |
Altri autori (Persone) |
DerGim J
BonavitoNino L |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Orbital mechanics
Celestial mechanics Astrodynamics |
ISBN |
1-60086-648-4
1-60086-429-5 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Cover; Title; Copyright; Foreword; Table of Contents; Preface; Introduction; Chapter 1 Newton's Laws; I. Newton's Laws of Motion; II. Newton's Law of Gravitation; III. The Gravitational Potential; IV. Gravitational Flux and Gauss' Theorem; V. Gravitational Properties of a True Sphere; Chapter 2 The Two-Body Problem; I. Reduction to the One-Center Problem; II. The One-Center Problem; III. The Laplace Vector; IV. The Conic Section Solutions; V. Elliptic Orbits; VI. Spherical Trigonometry; VII. Orbit in Space; VIII. Orbit Determination from Initial Values; Chapter 3 Lagrangian Dynamics
I. VariationsII. D'Alembert's Principle; III. Hamilton's Principle; IV. Lagrange's Equations; Reference; Chapter 4 The Hamiltonian Equations; I. An Important Theorem; II. Ignorable Variables; Chapter 5 Canonical Transformations; I. The Condition of Exact Differentials; II. Canonical Generating Functions; III. Extended Point Transformation; IV. Transformation from Plane Rectangular to Plane Polar Coordinates; V. The Jacobi Integral; References; Chapter 6 Hamilton-Jacobi Theory; I. The Hamilton-Jacobi Equation; II. An Important Special Case III. The Hamilton-Jacobi Equation for the Kepler ProblemIV. The Integrals for the Kepler Problem; V. Relations Connecting β[sub(2)] and β[sub(3)] with ω and Ω; VI. Summary; Bibliography; Chapter 7 Hamilton-Jacobi Perturbation Theory; Bibliography; Chapter 8 The Vinti Spheroidal Method for Satellite Orbits and Ballistic Trajectories; I. Introduction; II. The Coordinates and the Hamiltonian; III. The Hamilton-Jacobi Equation; IV. Laplace's Equation; V. Expansion of Potential in Spherical Harmonics; VI. Return to the HJ Equation; VII. The Kinematic Equations; VIII. Orbital Elements IX. Factoring the QuarticsX. The ρ Integrals; XI. The η Integrals; XII. The Mean Frequencies; XIII. Assembly of the Kinematic Equations; XIV. Solution of the Kinematic Equations; XV. The Periodic Terms; XVI. The Right Ascension Φ; XVII. Further Developments; References; Chapter 9 Delaunay Variables; Reference; Chapter 10 The Lagrange Planetary Equations; I. Semi-Major Axis; II. Eccentricity; III. Inclination; IV. Mean Anomaly; V. The Argument of Pericenter; VI. The Longitude of the Node; VII. Summary; Reference; Chapter 11 The Planetary Disturbing Function; Bibliography Chapter 12 Gaussian Variational Equations for the Jacobi ElementsReferences; Chapter 13 Gaussian Variational Equations for the Keplerian Elements; I. Preliminaries; II. Equations for α[sub(1)] and a; III. Equations for α[sub(2)] and e; IV. Equations for α[sub(3)] and I; V. Equations for β[sub(3)] = Ω; VI. Equations for β[sub(2)] = ω; VII. Equations for β[sub(1)] and l; VIII. Summary; Chapter 14 Potential Theory; I. Introduction; II. Laplace's Equation; III. The Eigenvalue Problem; IV. The R(r) Equation; V. The Assembled Solution; VI. Legendre Polynomials; VII. The Results for P[sub(n)](x) VIII. The 0 Solution for m > 0 |
Record Nr. | UNINA-9910781411803321 |
Vinti John P (John Pascal), <1907-> | ||
Reston, Va., : American Institute of Aeronautics and Astronautics, c1998 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Orbital and celestial mechanics [[electronic resource] /] / John P. Vinti ; edited by Gim J. Der, Nino L. Bonavito |
Autore | Vinti John P (John Pascal), <1907-> |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1998 |
Descrizione fisica | 1 online resource (415 p.) |
Disciplina | 629.4/113 |
Altri autori (Persone) |
DerGim J
BonavitoNino L |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Orbital mechanics
Celestial mechanics Astrodynamics |
ISBN |
1-60086-648-4
1-60086-429-5 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Cover; Title; Copyright; Foreword; Table of Contents; Preface; Introduction; Chapter 1 Newton's Laws; I. Newton's Laws of Motion; II. Newton's Law of Gravitation; III. The Gravitational Potential; IV. Gravitational Flux and Gauss' Theorem; V. Gravitational Properties of a True Sphere; Chapter 2 The Two-Body Problem; I. Reduction to the One-Center Problem; II. The One-Center Problem; III. The Laplace Vector; IV. The Conic Section Solutions; V. Elliptic Orbits; VI. Spherical Trigonometry; VII. Orbit in Space; VIII. Orbit Determination from Initial Values; Chapter 3 Lagrangian Dynamics
I. VariationsII. D'Alembert's Principle; III. Hamilton's Principle; IV. Lagrange's Equations; Reference; Chapter 4 The Hamiltonian Equations; I. An Important Theorem; II. Ignorable Variables; Chapter 5 Canonical Transformations; I. The Condition of Exact Differentials; II. Canonical Generating Functions; III. Extended Point Transformation; IV. Transformation from Plane Rectangular to Plane Polar Coordinates; V. The Jacobi Integral; References; Chapter 6 Hamilton-Jacobi Theory; I. The Hamilton-Jacobi Equation; II. An Important Special Case III. The Hamilton-Jacobi Equation for the Kepler ProblemIV. The Integrals for the Kepler Problem; V. Relations Connecting β[sub(2)] and β[sub(3)] with ω and Ω; VI. Summary; Bibliography; Chapter 7 Hamilton-Jacobi Perturbation Theory; Bibliography; Chapter 8 The Vinti Spheroidal Method for Satellite Orbits and Ballistic Trajectories; I. Introduction; II. The Coordinates and the Hamiltonian; III. The Hamilton-Jacobi Equation; IV. Laplace's Equation; V. Expansion of Potential in Spherical Harmonics; VI. Return to the HJ Equation; VII. The Kinematic Equations; VIII. Orbital Elements IX. Factoring the QuarticsX. The ρ Integrals; XI. The η Integrals; XII. The Mean Frequencies; XIII. Assembly of the Kinematic Equations; XIV. Solution of the Kinematic Equations; XV. The Periodic Terms; XVI. The Right Ascension Φ; XVII. Further Developments; References; Chapter 9 Delaunay Variables; Reference; Chapter 10 The Lagrange Planetary Equations; I. Semi-Major Axis; II. Eccentricity; III. Inclination; IV. Mean Anomaly; V. The Argument of Pericenter; VI. The Longitude of the Node; VII. Summary; Reference; Chapter 11 The Planetary Disturbing Function; Bibliography Chapter 12 Gaussian Variational Equations for the Jacobi ElementsReferences; Chapter 13 Gaussian Variational Equations for the Keplerian Elements; I. Preliminaries; II. Equations for α[sub(1)] and a; III. Equations for α[sub(2)] and e; IV. Equations for α[sub(3)] and I; V. Equations for β[sub(3)] = Ω; VI. Equations for β[sub(2)] = ω; VII. Equations for β[sub(1)] and l; VIII. Summary; Chapter 14 Potential Theory; I. Introduction; II. Laplace's Equation; III. The Eigenvalue Problem; IV. The R(r) Equation; V. The Assembled Solution; VI. Legendre Polynomials; VII. The Results for P[sub(n)](x) VIII. The 0 Solution for m > 0 |
Record Nr. | UNINA-9910825537503321 |
Vinti John P (John Pascal), <1907-> | ||
Reston, Va., : American Institute of Aeronautics and Astronautics, c1998 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
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 | ||
|
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 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
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-9910816720403321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2002 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Orbital mechanics and astrodynamics : techniques and tools for space missions / / Gerald R. Hintz |
Autore | Hintz Gerald R. |
Edizione | [Second edition.] |
Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , 2022 |
Descrizione fisica | 1 online resource (461 pages) |
Disciplina | 629.41 |
Soggetto topico |
Astrodynamics
Orbital mechanics |
ISBN |
9783030965730
9783030965723 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | 1. Fundamentals of Astrodynamics -- 2. Keplerian Motion -- 3. Orbital Maneuvers -- 4. Techniques of Astrodynamics -- 5. Non-Keplerian Motion -- 6. Spacecraft Rendezvous -- 7. Navigation and Mission Design Techniques and Tools -- 8. Changing from Mission Design to Flight Operations -- 9. Further Study. |
Record Nr. | UNINA-9910644266603321 |
Hintz Gerald R. | ||
Cham, Switzerland : , : Springer, , 2022 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Orbital mechanics and astrodynamics : techniques and tools for space missions / / Gerald R. Hintz |
Autore | Hintz Gerald R. |
Edizione | [Second edition.] |
Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , 2022 |
Descrizione fisica | 1 online resource (461 pages) |
Disciplina | 629.41 |
Soggetto topico |
Astrodynamics
Orbital mechanics |
ISBN |
9783030965730
9783030965723 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | 1. Fundamentals of Astrodynamics -- 2. Keplerian Motion -- 3. Orbital Maneuvers -- 4. Techniques of Astrodynamics -- 5. Non-Keplerian Motion -- 6. Spacecraft Rendezvous -- 7. Navigation and Mission Design Techniques and Tools -- 8. Changing from Mission Design to Flight Operations -- 9. Further Study. |
Record Nr. | UNISA-996508664303316 |
Hintz Gerald R. | ||
Cham, Switzerland : , : Springer, , 2022 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. di Salerno | ||
|