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Investigation Of Atmospheric Reentry For The Space Maneuver Vehicle
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Book Synopsis Investigation of Atmospheric Reentry for the Space Maneuver Vehicle by : Dennis J. McNabb
Download or read book Investigation of Atmospheric Reentry for the Space Maneuver Vehicle written by Dennis J. McNabb and published by . This book was released on 2004-03-01 with total page 95 pages. Available in PDF, EPUB and Kindle. Book excerpt: This study investigated the atmospheric reentry of the Space Maneuver Vehicle from low-earth orbit using an entry guidance concept similar to the Space Shuttle. The Space Maneuver Vehicle was modeled as a point mass with aerodynamic properties as determined using Newtonian impact theory. For the rarefied-flow transition regime bridging formulae are used to capture the effects of both hypersonic continuum flow and free molecular flow. Constraints to the reentry are developed and a reentry corridor is defined in the drag- velocity plane. Bank angle modulation is established as the primary means for controlling drag and range. The guidance concept is applied to both a high inclination orbit and a low inclination orbit with cross-range requirement. Monte Carlo error analysis validates the ability of the control algorithm to guide reentry in the presence of initial state errors, as well as atmospheric variations. (7 tables, 54 figures, 18 refs.)
Book Synopsis Investigation of Aerobraking to Return the Space Maneuver Vehicle to Low Earth Orbit from Geotransfer Orbit by : Benjamin M. Berlin
Download or read book Investigation of Aerobraking to Return the Space Maneuver Vehicle to Low Earth Orbit from Geotransfer Orbit written by Benjamin M. Berlin and published by . This book was released on 2005 with total page 202 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Performance Characteristics of Re-entry Vehicles by : Charles A. Bilbey
Download or read book Investigation of the Performance Characteristics of Re-entry Vehicles written by Charles A. Bilbey and published by . This book was released on 2005 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Study of a Guidance Scheme Using Approximate Solutions of Trajectory Equations to Control the Aerodynamic Skip Flight of a Reentry Vehicle by : Robert Scott Dunning
Download or read book Study of a Guidance Scheme Using Approximate Solutions of Trajectory Equations to Control the Aerodynamic Skip Flight of a Reentry Vehicle written by Robert Scott Dunning and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems by : Runqi Chai
Download or read book Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems written by Runqi Chai and published by Springer. This book was released on 2019-07-30 with total page 207 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book explores the design of optimal trajectories for space maneuver vehicles (SMVs) using optimal control-based techniques. It begins with a comprehensive introduction to and overview of three main approaches to trajectory optimization, and subsequently focuses on the design of a novel hybrid optimization strategy that combines an initial guess generator with an improved gradient-based inner optimizer. Further, it highlights the development of multi-objective spacecraft trajectory optimization problems, with a particular focus on multi-objective transcription methods and multi-objective evolutionary algorithms. In its final sections, the book studies spacecraft flight scenarios with noise-perturbed dynamics and probabilistic constraints, and designs and validates new chance-constrained optimal control frameworks. The comprehensive and systematic treatment of practical issues in spacecraft trajectory optimization is one of the book’s major features, making it particularly suited for readers who are seeking practical solutions in spacecraft trajectory optimization. It offers a valuable asset for researchers, engineers, and graduate students in GNC systems, engineering optimization, applied optimal control theory, etc.
Book Synopsis Dynamics of Atmospheric Re-Entry by : Frank J. Regan
Download or read book Dynamics of Atmospheric Re-Entry written by Frank J. Regan and published by AIAA. This book was released on 1993 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analytical Investigation of the Dynamic Behavior of a Nonlifting Manned Reentry Vehicle by : Jacob H. Lichtenstein
Download or read book Analytical Investigation of the Dynamic Behavior of a Nonlifting Manned Reentry Vehicle written by Jacob H. Lichtenstein and published by . This book was released on 1960 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Model Investigation of the Landing Characteristics of a Reentry Spacecraft with a Vertical-cylinder Air Bag for Load Alleviation by : John R. McGehee
Download or read book Model Investigation of the Landing Characteristics of a Reentry Spacecraft with a Vertical-cylinder Air Bag for Load Alleviation written by John R. McGehee and published by . This book was released on 1962 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Manual-control Simulation Study of a Nonlifting Vehicle During Orbit, Retro-rocket Firing, and Reentry Into the Earth's Atmosphere by : Roger M. Davidson
Download or read book Manual-control Simulation Study of a Nonlifting Vehicle During Orbit, Retro-rocket Firing, and Reentry Into the Earth's Atmosphere written by Roger M. Davidson and published by . This book was released on 1960 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Motion and Heating During Atmosphere Reentry of Space Vehicles by : Thomas J. Wong
Download or read book Motion and Heating During Atmosphere Reentry of Space Vehicles written by Thomas J. Wong and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 by : Dennis E. Fuller
Download or read book Static Stability Investigations of Proposed Project Fire Space-vehicle and Reentry-package Configurations at Mach Numbers from 1.47 to 4.63 written by Dennis E. Fuller and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Aerodynamic Surfaces Versus Thrust Maneuvers on Reentry Vehicles by : Meredith M. Albrecht
Download or read book The Effect of Aerodynamic Surfaces Versus Thrust Maneuvers on Reentry Vehicles written by Meredith M. Albrecht and published by . This book was released on 2005 with total page 146 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Advanced Research by : Langley Research Center
Download or read book Advanced Research written by Langley Research Center and published by . This book was released on 1964 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Limiting Future Collision Risk to Spacecraft by : National Research Council
Download or read book Limiting Future Collision Risk to Spacecraft written by National Research Council and published by National Academies Press. This book was released on 2011-12-16 with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt: Derelict satellites, equipment and other debris orbiting Earth (aka space junk) have been accumulating for many decades and could damage or even possibly destroy satellites and human spacecraft if they collide. During the past 50 years, various National Aeronautics and Space Administration (NASA) communities have contributed significantly to maturing meteoroid and orbital debris (MMOD) programs to their current state. Satellites have been redesigned to protect critical components from MMOD damage by moving critical components from exterior surfaces to deep inside a satellite's structure. Orbits are monitored and altered to minimize the risk of collision with tracked orbital debris. MMOD shielding added to the International Space Station (ISS) protects critical components and astronauts from potentially catastrophic damage that might result from smaller, untracked debris and meteoroid impacts. Limiting Future Collision Risk to Spacecraft: An Assessment of NASA's Meteoroid and Orbital Debris Program examines NASA's efforts to understand the meteoroid and orbital debris environment, identifies what NASA is and is not doing to mitigate the risks posed by this threat, and makes recommendations as to how they can improve their programs. While the report identified many positive aspects of NASA's MMOD programs and efforts including responsible use of resources, it recommends that the agency develop a formal strategic plan that provides the basis for prioritizing the allocation of funds and effort over various MMOD program needs. Other necessary steps include improvements in long-term modeling, better measurements, more regular updates of the debris environmental models, and other actions to better characterize the long-term evolution of the debris environment.
Book Synopsis Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180° by : J. W. Usry
Download or read book Investigation of the Static Stability Characteristics of a Reentry Spacecraft Model in Free Flight for Mach Numbers from 2.62 to 1.11 Launched at an Angle of Attack of 180° written by J. W. Usry and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Space Vehicle Dynamics and Control by : Bong Wie
Download or read book Space Vehicle Dynamics and Control written by Bong Wie and published by AIAA. This book was released on 1998 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt: A textbook that incorporates the latest methods used for the analysis of spacecraft orbital, attitude, and structural dynamics and control. Spacecraft dynamics is treated as a dynamic system with emphasis on practical applications, typical examples of which are the analysis and redesign of the pointing control system of the Hubble Space Telescope and the analysis of an active vibrations control for the COFS (Control of Flexible Structures) Mast Flight System. In addition to the three subjects mentioned above, dynamic systems modeling, analysis, and control are also discussed. Annotation copyrighted by Book News, Inc., Portland, OR
Author :Committee on Reusable Launch Vehicle Technology and Test Program Publisher :National Academies Press ISBN 13 :0309588960 Total Pages :99 pages Book Rating :4.3/5 (95 download)
Book Synopsis Reusable Launch Vehicle by : Committee on Reusable Launch Vehicle Technology and Test Program
Download or read book Reusable Launch Vehicle written by Committee on Reusable Launch Vehicle Technology and Test Program and published by National Academies Press. This book was released on 1996-01-22 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt: The key to opening the use of space to private enterprise and to broader public uses lies in reducing the cost of the transportation to space. More routine, affordable access to space will entail aircraft-like quick turnaround and reliable operations. Currently, the space Shuttle is the only reusable launch vehicle, and even parts of it are expendable while other parts require frequent and extensive refurbishment. NASA's highest priority new activity, the Reusable Launch Vehicle program, is directed toward developing technologies to enable a new generation of space launchers, perhaps but not necessarily with single stage to orbit capability. This book assesses whether the technology development, test and analysis programs in propulsion and materials-related technologies are properly constituted to provide the information required to support a December 1996 decision to build the X-33, a technology demonstrator vehicle; and suggest, as appropriate, necessary changes in these programs to ensure that they will support vehicle feasibility goals.
