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Advances in Spacecraft Systems and Orbit Determination / / edited by Rushi Ghadawala
| Advances in Spacecraft Systems and Orbit Determination / / edited by Rushi Ghadawala |
| Pubbl/distr/stampa | Rijeka, Croatia : , : IntechOpen, , 2012 |
| Descrizione fisica | 1 online resource (278 pages) : illustrations some color |
| Disciplina | 629.41 |
| Soggetto topico |
Space vehicles - Orbits
Space vehicles - Control systems Space trajectories |
| ISBN | 953-51-6169-5 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910138264303321 |
| Rijeka, Croatia : , : IntechOpen, , 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Application of the Lambert Problem to inverse-square gravity [[electronic resource] /] / by Isaac Sofair
| Application of the Lambert Problem to inverse-square gravity [[electronic resource] /] / by Isaac Sofair |
| Autore | Sofair Isaac |
| Pubbl/distr/stampa | Dahlgren, Va. : , : Dahlgren Division, Naval Surface Warfare Center, , [2003] |
| Descrizione fisica | 1 volume (various paging) : digital, PDF file |
| Collana | NSWCDD/TR |
| Soggetto topico |
Aeronautics
Astronautics Space trajectories |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910694679603321 |
Sofair Isaac
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| Dahlgren, Va. : , : Dahlgren Division, Naval Surface Warfare Center, , [2003] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flight investigation of the effects of Apollo heat-shield singularities on ablator performance / / by Thomas E. Walton, Jr., William G. Witte, and Brian J. O'Hare
| Flight investigation of the effects of Apollo heat-shield singularities on ablator performance / / by Thomas E. Walton, Jr., William G. Witte, and Brian J. O'Hare |
| Autore | Walton Thomas E. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , September 1968 |
| Descrizione fisica | 1 online resource (60 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Ablative materials
Space trajectories Aerodynamics Materials at high temperatures |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715055003321 |
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Walton Thomas E.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , September 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Redundant inertial measurement unit reconfiguration and trajectory replanning of launch vehicle / / Xuefeng Li, Fan Xu and Guoqiang Xu
| Redundant inertial measurement unit reconfiguration and trajectory replanning of launch vehicle / / Xuefeng Li, Fan Xu and Guoqiang Xu |
| Autore | Li Xuefeng |
| Pubbl/distr/stampa | Gateway East, Singapore : , : Springer, , [2022] |
| Descrizione fisica | 1 online resource (196 pages) |
| Disciplina | 531.12 |
| Collana | Navigation: Science and Technology |
| Soggetto topico |
Launch vehicles (Astronautics)
Inertia (Mechanics) Space trajectories |
| ISBN | 981-19-4637-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Intro -- Foreword -- Preface -- Contents -- 1 Introduction -- 1.1 Redundant Reconfiguration After IMU Failure -- 1.2 Trajectory Re-planning After Propulsion System Failure -- 2 Model of Launch Vehicle Dynamics and Redundant Strapdown IMUs -- 2.1 Dynamics Model -- 2.1.1 Coordinate System -- 2.1.2 Mechanics Model -- 2.1.3 Centroid Dynamics and Kinematics Equations -- 2.1.4 Description of Orbit -- 2.1.5 Characteristic Orbit Parameters -- 2.2 Redundant Strapdown IMUs Modeling and Analysis -- 2.2.1 Model of Redundant Gyro Error -- 2.2.2 Model of Redundant Accelerometer Error -- 2.2.3 Model of Reconfiguration Parameters -- 3 Optimal Control Problems and Common Solutions -- 3.1 Optimal Control Model -- 3.1.1 Optimal Control Problem -- 3.1.2 Solution to Optimal Control Problem -- 3.2 Nonlinear Programming (NLP) Model -- 3.2.1 Unconstrained Optimization Problems -- 3.2.2 Constrained Optimization Problem -- 3.3 Convex Optimization Problem -- 3.3.1 Dual Theory of Convex Optimization -- 3.3.2 Optimality Condition -- 3.4 Nonlinear Programming Algorithms -- 3.4.1 SQP Algorithm -- 3.4.2 Interior-Point Method -- 3.4.3 Solving Problems -- 3.5 Convex Optimization Algorithms -- 3.6 Summary -- 4 Redundant IMU Fault Detection -- 4.1 Scheme of Redundant IMU Configuration -- 4.1.1 Index of Redundant Configuration -- 4.1.2 Analysis of Redundant Configuration Architecture -- 4.2 Diagnosis for Redundant Configuration -- 4.2.1 Vote Method -- 4.2.2 Parity Vector Method -- 4.3 Summary -- 5 Redundant IMU Reconfiguration -- 5.1 Typical Parity Check Method -- 5.2 Single-Set Multi-meter Crossover Reconfiguration -- 5.3 Reconfiguration Strategy of Engineering Application -- 5.3.1 Triple Redundancy Reconfiguration Strategy -- 5.3.2 Single-Set Five-Gyro Five-Accelerometer Reconfiguration Strategy -- 5.4 Summary -- 6 Trajectory Re-planning.
6.1 Theoretical Analysis of Mission Partitions -- 6.1.1 Estimation of Apogee Altitude and Orbit Inclination -- 6.1.2 Adaptive Orbit Entry Conditions -- 6.1.3 Re-planning Orbit Entry Conditions -- 6.1.4 Downgrade Mission Orbit Entry Conditions -- 6.1.5 Design of Mission Partitions -- 6.2 Off-Line Trajectory Planning -- 6.2.1 Off-Line Planning and Design -- 6.2.2 Adaptive Pseudospectral Method (PSM) -- 6.2.3 Solution to Off-Line Planning Problems -- 6.2.4 Planned Trajectory Interpolation -- 6.2.5 Simulation Analysis -- 6.3 On-Line Trajectory Planning -- 6.3.1 On-Line Planning and Design -- 6.3.2 Concept of Convex Optimization Problem -- 6.3.3 Variable Substitution and Relaxation -- 6.3.4 Conversion of Convex Optimization Problem -- 6.3.5 On-Line Planning Problem Solving -- 6.3.6 Simulation Analysis -- 6.4 Summary -- 7 Multistage Rocket Trajectory Re-planning -- 7.1 Rocket Trajectory Planning -- 7.2 Simulation of Stage-I Operation Propulsion System Failure -- 7.2.1 Re-planning Orbit Entry Design (Enter Partition B: I-B After Failure at Stage-I) -- 7.2.2 Re-planning Downgrade Design (Enter Partition C: I-C After Failure at Stage-I) -- 7.3 Simulation of Propulsion System Failure During Stage-II Operation -- 7.3.1 Re-planning Orbit Entry Design (Enter Partition B: II-B After Failure at Stage-II) -- 7.3.2 Re-planning Downgrade Design (Enter Partition C: II-C After Failure at Stage-II) -- 7.4 Summary -- Postscript -- Bibliography. |
| Record Nr. | UNINA-9910627239003321 |
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Li Xuefeng
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| Gateway East, Singapore : , : Springer, , [2022] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Research in space science
| Research in space science |
| Pubbl/distr/stampa | Washington, D.C. : , : Smithsonian Institution, , 1963 |
| Descrizione fisica | 1 online resource (242 pages) : illustrations, maps |
| Collana | Smithsonian contributions to astrophysics |
| Soggetto topico |
Artificial satellites
Space trajectories Geophysics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709796203321 |
| Washington, D.C. : , : Smithsonian Institution, , 1963 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Round trip trajectories with stopovers at both Mars and Venus / / by E.A. Willis, Jr. and J.A. Padrutt
| Round trip trajectories with stopovers at both Mars and Venus / / by E.A. Willis, Jr. and J.A. Padrutt |
| Autore | Willis Edward A. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, , 1969 |
| Descrizione fisica | 1 online resource (approximately 11 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Space trajectories
Interplanetary voyages Trajectories Mars (planet) Venus (planet) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716800703321 |
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Willis Edward A.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, , 1969 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A semigraphical method for a deorbit trajectory design study / / by Richard N. Green, William F. Hampshire II, and Sue W. Souders
| A semigraphical method for a deorbit trajectory design study / / by Richard N. Green, William F. Hampshire II, and Sue W. Souders |
| Autore | Green Richard N. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 |
| Descrizione fisica | 1 online resource (23 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico | Space trajectories |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715011803321 |
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Green Richard N.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Simplified technique for determining pericynthion altitude of lunar orbits / / by L. Keith Barker
| Simplified technique for determining pericynthion altitude of lunar orbits / / by L. Keith Barker |
| Autore | Barker L. Keith |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 |
| Descrizione fisica | 1 online resource (13 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Orbital transfer (Space flight)
Space trajectories |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714051203321 |
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Barker L. Keith
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| Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
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Space trajectories
(8)
- Ablative materials (1)
- Aerodynamics (1)
- Aeronautics (1)
- Artificial satellites (1)