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Analytical Solutions for Extremal Space Trajectories

Analytical Solutions for Extremal Space Trajectories
  • Author : Dilmurat M. Azimov
  • Publisher : Butterworth-Heinemann
  • Release : 23 August 2017
GET THIS BOOKAnalytical Solutions for Extremal Space Trajectories

Analytical Solutions for Extremal Space Trajectories presents an overall treatment of the general optimal control problem, in particular, the Mayer’s variational problem, with necessary and sufficient conditions of optimality. It also provides a detailed derivation of the analytical solutions of these problems for thrust arcs for the Newtonian, linear central and uniform gravitational fields. These solutions are then used to analytically synthesize the extremal and optimal trajectories for the design of various orbital transfer and powered descent and landing

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Advanced Problems and Methods for Space Flight Optimization

Advanced Problems and Methods for Space Flight Optimization
  • Author : B. Fraeijs De Veubeke
  • Publisher : Elsevier
  • Release : 22 October 2013
GET THIS BOOKAdvanced Problems and Methods for Space Flight Optimization

Advanced Problems and Methods for Space Flight Optimization presents the optimization theory and its application to space flight. This book covers a wide range of topics, including optimal guidance, general mathematical methods of optimization, optimal transfer trajectories, and optimization of design parameters. Organized into 15 chapters, this book begins with an overview of the approximate analytic solution developed for minimum fuel guidance from an arbitrary point on a hyperbolic orbit into a definite circular orbit. This text then determines the maximum

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Rigid Body Dynamics for Space Applications

Rigid Body Dynamics for Space Applications
  • Author : Vladimir S Aslanov
  • Publisher : Butterworth-Heinemann
  • Release : 22 April 2017
GET THIS BOOKRigid Body Dynamics for Space Applications

Rigid Body Dynamics for Space Applications explores the modern problems of spaceflight mechanics, such as attitude dynamics of re-entry and space debris in Earth's atmosphere; dynamics and control of coaxial satellite gyrostats; deployment, dynamics, and control of a tether-assisted return mission of a re-entry capsule; and removal of large space debris by a tether tow. Most space systems can be considered as a system of rigid bodies, with additional elastic and viscoelastic elements and fuel residuals in some cases. This

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Spacecraft Trajectory Optimization

Spacecraft Trajectory Optimization
  • Author : Bruce A. Conway
  • Publisher : Cambridge University Press
  • Release : 23 August 2010
GET THIS BOOKSpacecraft Trajectory Optimization

This is a long-overdue volume dedicated to space trajectory optimization. Interest in the subject has grown, as space missions of increasing levels of sophistication, complexity, and scientific return - hardly imaginable in the 1960s - have been designed and flown. Although the basic tools of optimization theory remain an accepted canon, there has been a revolution in the manner in which they are applied and in the development of numerical optimization. This volume purposely includes a variety of both analytical

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