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Trajectories Of Launch And Reentry Systems


Trajectories Of Launch And Reentry Systems
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Trajectories Of Launch And Reentry Systems


Trajectories Of Launch And Reentry Systems
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Author : Paolo Teofilatto
language : en
Publisher: Springer Nature
Release Date : 2024-12-26

Trajectories Of Launch And Reentry Systems written by Paolo Teofilatto and has been published by Springer Nature this book supported file pdf, txt, epub, kindle and other format this book has been release on 2024-12-26 with Technology & Engineering categories.


This book examines ascent trajectories of space launch vehicles and re-entry trajectories of space capsules. The decommissioned SCOUT is used as a reference launcher and the reader will be introduced to various and detailed aspects of a launch vehicle that are not generally available in the literature, since this information is limited to internal industry and agency reports. The SCOUT data are used here as a study case and the reader will be able to generate a complete numerical code using the general equations of flight introduced in different reference systems, including the time-dependent parameters representing the launcher and its environment with a high degree of accuracy. The guidance parameters for injection into orbits of different semiaxes, eccentricities and inclinations are determined by guessed values obtained by original analytical formulae. These formulae allow a fast and sufficiently accurate design of the rocket trajectory within the atmosphere; in the exo-atmospheric flight closed form solutions of the optimal problem of injection into orbit are provided. The second part of the book deals with re-entry trajectories. Basic analytical formulae for ballistic reentry are presented to evaluate the reentry trajectory and the capsule design in terms of critical parameters such as temperature and load peak. Entry corridors for ballistic reentry trajectories are then determined for various planets with atmospheres. The effect of lift is analysed to increase the entry corridors and guide the capsule to a target landing point. Autonomous and real-time guidance algorithms are developed for capsule of low aerodynamic efficiency and winged re-entry vehicles.



Scientific And Technical Aerospace Reports


Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1994

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aeronautics categories.




Through Optimization Of Aerospace Vehicle Trajectories By The Pontryagin Maximum Principle


Through Optimization Of Aerospace Vehicle Trajectories By The Pontryagin Maximum Principle
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Author : Alexander S. Filatyev
language : en
Publisher: Springer Nature
Release Date : 2025-05-28

Through Optimization Of Aerospace Vehicle Trajectories By The Pontryagin Maximum Principle written by Alexander S. Filatyev and has been published by Springer Nature this book supported file pdf, txt, epub, kindle and other format this book has been release on 2025-05-28 with Technology & Engineering categories.


This monograph investigates the trajectory optimization problems of low- and finite-thrust aerospace vehicles and spacecraft using an indirect method based on the Pontryagin maximum principle, providing a methodological basis for the construction of numerical techniques that are superior in versatility and accuracy to direct methods. This book provides a theoretical explanation of the approaches used and also an extensive gallery of the results of practical numerical studies. The problem of boundary value problem convergence has been largely overcome, which has made it possible to practically automate the optimization of trajectories and to achieve a qualitative generalization with a number of fundamentally new results. Examples of practical optimization of branching trajectories of complex dynamics systems with finite and continual sets of branches, in deterministic and stochastic statements, with control constraints and phase constraints of various orders are demonstrated. An emphasis is placed on the consistent application of methods of numerical continuation with respect to a parameter to solve various problems in the flight mechanics of spacecraft with an electric propulsion system (EPS). The problems considered include the optimization of direct interplanetary flights of spacecraft with thrusters having limited power or limited thrust, of interplanetary flights of such spacecraft using gravity assisted maneuvers, of multi-orbit interorbital transfers of spacecraft with limited-thrust EPS. As a result, it was possible to develop a set of numerical continuation methods for solving a wide range of optimization problems for spacecraft trajectories with EPS with improved characteristics in terms of convergence and performance. This monograph also contains a description of many pitfalls in solving a wide range of problems of optimizing the trajectories of aerospace vehicles and recipes for effectively overcoming them.



Technical Abstract Bulletin


Technical Abstract Bulletin
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Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1964

Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Military art and science categories.




Nasa Technical Note


Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1964

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aeronautics categories.




The Nasa Scientific And Technical Information System Its Scope And Coverage


The Nasa Scientific And Technical Information System Its Scope And Coverage
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Author :
language : en
Publisher:
Release Date : 1988

The Nasa Scientific And Technical Information System Its Scope And Coverage written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1988 with Aeronautics categories.




U S Government Research Development Reports


U S Government Research Development Reports
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Author :
language : en
Publisher:
Release Date : 1970

U S Government Research Development Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Science categories.




Nasa Scientific And Technical Reports


Nasa Scientific And Technical Reports
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Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
language : en
Publisher:
Release Date : 1967

Nasa Scientific And Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Aeronautics categories.




Optimal Trajectories In Atmospheric Flight


Optimal Trajectories In Atmospheric Flight
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Author : Nguyen Vinh
language : en
Publisher: Elsevier
Release Date : 2012-12-02

Optimal Trajectories In Atmospheric Flight written by Nguyen Vinh and has been published by Elsevier this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-12-02 with Technology & Engineering categories.


Optimal Trajectories in Atmospheric Flight deals with the optimization of trajectories in atmospheric flight. The book begins with a simple treatment of functional optimization followed by a discussion of switching theory. It then presents the derivation of the general equations of motion along with the basic knowledge in aerodynamics and propulsion necessary for the analysis of atmospheric flight trajectories. It goes on to the study of optimal trajectories by providing the general properties of the optimal aerodynamic controls and the integrals of motion. This is followed by discussions of high subsonic and supersonic flight, and approximation techniques to reduce the order of the problem for a fast computation of the optimal trajectory. The final chapters present analyses of optimal reentry trajectories and orbital maneuvers. This book is intended as a reference text for scientists and engineers wanting to get into the subject of optimal trajectories in atmospheric flight. If used for teaching purposes, the book is written in a self-contained way so that a selective use of the material is at the discretion of the lecturer. The first 11 chapters are sufficient for a one-semester course with emphasis on optimal maneuvers of high performance aircraft.



Hypersonic Airbreathing Propulsion


Hypersonic Airbreathing Propulsion
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Author : William H. Heiser
language : en
Publisher: AIAA
Release Date : 1994

Hypersonic Airbreathing Propulsion written by William H. Heiser and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Science categories.


An almost entirely self-contained engineering textbook primarily for use in undergraduate and graduate courses in airbreathing propulsion. It provides a broad and basic introduction to the elements needed to work in the field as it develops and grows. Homework problems are provided for almost every individual subject. An extensive array of PC-based user-friendly computer programs is provided in order to facilitate repetitious and/or complex calculations. Annotation copyright by Book News, Inc., Portland, OR