Dynamics and simulation of flexible rockets /
Dynamics and Simulation of Flexible Rockets provides a full state, multiaxis treatment of launch vehicle flight mechanics and provides the state equations in a format that can be readily coded into a simulation environment. Various forms of the mass matrix for the vehicle dynamics are presented. The...
| Main Authors: | , , |
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| Format: | software, multimedia |
| Language: | eng |
| Published: |
Amsterdam : Academic Press,
2021
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| Subjects: | |
| Online Access: | https://www.sciencedirect.com/science/book/9780128199947 |
| _version_ | 1826472392138948608 |
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| author | Barrows, Timothy M., author 650757 Orr, Jeb S., author 650758 ScienceDirect (Online service) 7722 |
| author_facet | Barrows, Timothy M., author 650757 Orr, Jeb S., author 650758 ScienceDirect (Online service) 7722 |
| author_sort | Barrows, Timothy M., author 650757 |
| collection | OCEAN |
| description | Dynamics and Simulation of Flexible Rockets provides a full state, multiaxis treatment of launch vehicle flight mechanics and provides the state equations in a format that can be readily coded into a simulation environment. Various forms of the mass matrix for the vehicle dynamics are presented. The book also discusses important forms of coupling, such as between the nozzle motions and the flexible body.This book is designed to help practicing aerospace engineers create simulations that can accurately verify that a space launch vehicle will successfully perform its mission. Much of the open literature on rocket dynamics is based on analysis techniques developed during the Apollo program of the 1960s. Since that time, large-scale computational analysis techniques and improved methods for generating Finite Element Models (FEMs) have been developed. The art of the problem is to combine the FEM with dynamic models of separate elements such as sloshing fuel and moveable engine nozzles. The pitfalls that may occur when making this marriage are examined in detail. |
| first_indexed | 2024-03-05T17:17:45Z |
| format | software, multimedia |
| id | KOHA-OAI-TEST:605642 |
| institution | Universiti Teknologi Malaysia - OCEAN |
| language | eng |
| last_indexed | 2024-03-05T17:17:45Z |
| publishDate | 2021 |
| publisher | Amsterdam : Academic Press, |
| record_format | dspace |
| spelling | KOHA-OAI-TEST:6056422023-09-12T08:19:05ZDynamics and simulation of flexible rockets / Barrows, Timothy M., author 650757 Orr, Jeb S., author 650758 ScienceDirect (Online service) 7722 software, multimedia Electronic books 631902 Amsterdam : Academic Press,©20212021engDynamics and Simulation of Flexible Rockets provides a full state, multiaxis treatment of launch vehicle flight mechanics and provides the state equations in a format that can be readily coded into a simulation environment. Various forms of the mass matrix for the vehicle dynamics are presented. The book also discusses important forms of coupling, such as between the nozzle motions and the flexible body.This book is designed to help practicing aerospace engineers create simulations that can accurately verify that a space launch vehicle will successfully perform its mission. Much of the open literature on rocket dynamics is based on analysis techniques developed during the Apollo program of the 1960s. Since that time, large-scale computational analysis techniques and improved methods for generating Finite Element Models (FEMs) have been developed. The art of the problem is to combine the FEM with dynamic models of separate elements such as sloshing fuel and moveable engine nozzles. The pitfalls that may occur when making this marriage are examined in detail.Includes bibliographical references and index1. Introduction -- 2. The system mass matrix -- 3. Slosh modeling -- 4. Pendulum model -- 5. Forces and torques -- 6. Engine interactions -- 7. Linearization -- 8. Simulation parameters -- 9. Stability and control -- 10. Implementation and analysis.Dynamics and Simulation of Flexible Rockets provides a full state, multiaxis treatment of launch vehicle flight mechanics and provides the state equations in a format that can be readily coded into a simulation environment. Various forms of the mass matrix for the vehicle dynamics are presented. The book also discusses important forms of coupling, such as between the nozzle motions and the flexible body.This book is designed to help practicing aerospace engineers create simulations that can accurately verify that a space launch vehicle will successfully perform its mission. Much of the open literature on rocket dynamics is based on analysis techniques developed during the Apollo program of the 1960s. Since that time, large-scale computational analysis techniques and improved methods for generating Finite Element Models (FEMs) have been developed. The art of the problem is to combine the FEM with dynamic models of separate elements such as sloshing fuel and moveable engine nozzles. The pitfalls that may occur when making this marriage are examined in detail.Rockets (Aeronautics)Rocketryhttps://www.sciencedirect.com/science/book/9780128199947URN:ISBN:9780128199947Remote access restricted to users with a valid UTM ID via VPN. |
| spellingShingle | Rockets (Aeronautics) Rocketry Barrows, Timothy M., author 650757 Orr, Jeb S., author 650758 ScienceDirect (Online service) 7722 Dynamics and simulation of flexible rockets / |
| title | Dynamics and simulation of flexible rockets / |
| title_full | Dynamics and simulation of flexible rockets / |
| title_fullStr | Dynamics and simulation of flexible rockets / |
| title_full_unstemmed | Dynamics and simulation of flexible rockets / |
| title_short | Dynamics and simulation of flexible rockets / |
| title_sort | dynamics and simulation of flexible rockets |
| topic | Rockets (Aeronautics) Rocketry |
| url | https://www.sciencedirect.com/science/book/9780128199947 |
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