Orbital Relative Motion And Terminal Rendezvous

Author : Jean Albert Kéchichian
Publisher : Unknown
Page : 0 pages
File Size : 54,5 Mb
Release : 2021
Category : Electronic
ISBN : 3030646580

Get Book

Orbital Relative Motion and Terminal Rendezvous by Jean Albert Kéchichian Pdf

This book provides a comprehensive analysis of time-fixed terminal rendezvous around the Earth using chemical propulsion. The book has two main objectives. The first is to derive the mathematics of relative motion in near-circular orbit when subjected to perturbations emanating from the oblateness of the Earth, third-body gravity, and atmospheric drag. The mathematics are suitable for quick trajectory prediction and the creation of computer codes and efficient software to solve impulsive maneuvers and fly rendezvous missions. The second objective of this book is to show how the relative motion theory is applied to the exact precision-integrated, long-duration, time-fixed terminal rendezvous problem around the oblate Earth for the general elliptic orbit case. The contents are both theoretical and applied, with long-lasting value for aerospace engineers, trajectory designers, professors of orbital mechanics, and students at the graduate level and above. .

Author : Jean Albert Kéchichian
Publisher : Springer Nature
Page : 417 pages
File Size : 49,6 Mb
Release : 2021-04-12
Category : Technology & Engineering
ISBN : 9783030646578

Get Book

Orbital Relative Motion and Terminal Rendezvous by Jean Albert Kéchichian Pdf

This book provides a comprehensive analysis of time-fixed terminal rendezvous around the Earth using chemical propulsion. The book has two main objectives. The first is to derive the mathematics of relative motion in near-circular orbit when subjected to perturbations emanating from the oblateness of the Earth, third-body gravity, and atmospheric drag. The mathematics are suitable for quick trajectory prediction and the creation of computer codes and efficient software to solve impulsive maneuvers and fly rendezvous missions. The second objective of this book is to show how the relative motion theory is applied to the exact precision-integrated, long-duration, time-fixed terminal rendezvous problem around the oblate Earth for the general elliptic orbit case. The contents are both theoretical and applied, with long-lasting value for aerospace engineers, trajectory designers, professors of orbital mechanics, and students at the graduate level and above.

Author : Ye Yan,Xu Huang,Yueneng Yang
Publisher : Springer
Page : 148 pages
File Size : 42,6 Mb
Release : 2016-10-25
Category : Technology & Engineering
ISBN : 9789811026034

Get Book

Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion by Ye Yan,Xu Huang,Yueneng Yang Pdf

This book develops a dynamical model of the orbital motion of Lorentz spacecraft in both unperturbed and J2-perturbed environments. It explicitly discusses three kinds of typical space missions involving relative orbital control: spacecraft hovering, rendezvous, and formation flying. Subsequently, it puts forward designs for both open-loop and closed-loop control schemes propelled or augmented by the geomagnetic Lorentz force. These control schemes are entirely novel and represent a significantly departure from previous approaches.

Author : Harold Hornby
Publisher : Unknown
Page : 44 pages
File Size : 51,9 Mb
Release : 1962
Category : Satellites
ISBN : UIUC:30112106592642

Get Book

An Analytical Study of Orbital Rendezvous for Least Fuel and Least Energy by Harold Hornby Pdf

Author : D. F. Bender,A. L. Blackford
Publisher : Unknown
Page : 89 pages
File Size : 40,5 Mb
Release : 1968
Category : Electronic
ISBN : OCLC:254215872

Get Book

Relative Motion, Guidance Equations for Terminal Rendezvous by D. F. Bender,A. L. Blackford Pdf

Author : John M. Eggleston
Publisher : Unknown
Page : 48 pages
File Size : 44,5 Mb
Release : 1962
Category : Satellites
ISBN : UIUC:30112106590851

Get Book

A Study of the Optimum Velocity Change to Intercept and Rendezvous by John M. Eggleston Pdf

Author : John F. Price,A. K. Dunlap
Publisher : Unknown
Page : 294 pages
File Size : 47,7 Mb
Release : 1963
Category : Orbital rendezvous (Space flight)
ISBN : UVA:X000755267

Get Book

Rendezvous and Orbital Docking by John F. Price,A. K. Dunlap Pdf

Author : Richard A. Hord,Barbara J. Durling
Publisher : Unknown
Page : 48 pages
File Size : 40,6 Mb
Release : 1961
Category : Linear systems
ISBN : UIUC:30112106590513

Get Book

Analysis of a Linear System for Variable-thrust Control in the Terminal Phase of Rendezvous by Richard A. Hord,Barbara J. Durling Pdf

A linear system for applying thrust to a ferry vehicle in the 3 terminal phase of rendezvous with a satellite is analyzed. This system requires that the ferry thrust vector per unit mass be variable and equal to a suitable linear combination of the measured position and velocity vectors of the ferry relative to the satellite. The variations of the ferry position, speed, acceleration, and mass ratio are examined for several combinations of the initial conditions and two basic control parameters analogous to the undamped natural frequency and the fraction of critical damping. Upon making a desirable selection of one control parameter and requiring minimum fuel expenditure for given terminal-phase initial conditions, a simplified analysis in one dimension practically fixes the choice of the remaining control parameter. The system can be implemented by an automatic controller or by a pilot.

Author : Edgar C. Lineberry,Edwin C. Foudriat,United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 40 pages
File Size : 48,8 Mb
Release : 1962
Category : Navigation
ISBN : UIUC:30112106908954

Get Book

Study of an Automatic System for Control of the Terminal Phase of Satellite Rendezvous by Edgar C. Lineberry,Edwin C. Foudriat,United States. National Aeronautics and Space Administration Pdf

An analytical and simulation study was conducted of an automatic system to control the terminal phase of rendezvous between two space vehicles. The system employs switching and thrust orientation criteria based upon relative-motion parameters first to establish a collision course and then to reduce the range and range rate to zero simultaneously. Techniques are developed for employing either modulated thrust or on-off thrust at a constant level. Results of the study indicate that the automatic system can effectively control rendezvous over a wide range of initial conditions and can utilize the available fuel in a very efficient manner.

Author : Terrance M. Carney
Publisher : Unknown
Page : 72 pages
File Size : 43,7 Mb
Release : 1961
Category : Guidance systems (Flight)
ISBN : UIUC:30112106872333

Get Book

An Automatic Terminal Guidance System for Rendezvous with a Satellite by Terrance M. Carney Pdf

Author : Vladimir A. Chobotov
Publisher : AIAA
Page : 490 pages
File Size : 40,7 Mb
Release : 2002
Category : Artificial satellites
ISBN : 1600860974

Get Book

Orbital Mechanics by Vladimir A. Chobotov Pdf

Annotation Designed to be used as a graduate student textbook and a ready reference for the busy professional, this third edition of "Orbital Mechanics is structured so that you can easily look up the things you need to know. This edition includes more recent developments in space exploration (e.g. Galileo, Cassini, Mars Odyssey missions). Also, the chapter on space debris was rewritten to reflect new developments in that area. The well-organized chapters cover every basic aspect of orbital mechanics, from celestial relationships to the problems of space debris. The book is clearly written in language familiar to aerospace professionals and graduate students, with all of the equations, diagrams, and graphs you would like to have close at hand. An updated software package on CD-ROM includes: HW Solutions, which presents a range of viewpoints and guidelines for solving selected problems in the text; Orbital Calculator, which provides an interactive environment for the generation of Keplerian orbits, orbital transfer maneuvers, and animation of ellipses, hyperbolas, 'and interplanetary orbits; and Orbital Mechanics Solutions

Author : John Marshall Eggleston,Harold D. Beck
Publisher : Unknown
Page : 52 pages
File Size : 48,5 Mb
Release : 1961
Category : Equations of motion
ISBN : NASA:31769000421332

Get Book

A Study of the Positions and Velocities of a Space Station and a Ferry Vehicle During Rendezvous and Return by John Marshall Eggleston,Harold D. Beck Pdf

A study is made of the families of nonthrusting ascent trajectories during rendezvous with an orbiting space station and the descent trajectories to the earth's atmosphere. Equations of motion are derived and results are shown for two typical orbits of the station (one circular and one elliptic orbit). Boundaries of launch (at time of booster burnout) and rendezvous conditions are given and the effects of delays in launch time are discussed.

Author : Afonso Botelho,Baltazar Parreira,Paulo N. Rosa,João Miranda Lemos
Publisher : Springer Nature
Page : 116 pages
File Size : 46,6 Mb
Release : 2021-06-24
Category : Technology & Engineering
ISBN : 9783030756963

Get Book

Predictive Control for Spacecraft Rendezvous by Afonso Botelho,Baltazar Parreira,Paulo N. Rosa,João Miranda Lemos Pdf

This brief addresses the design of model predictive control algorithms for performing space rendezvous manoeuvres. It consolidates developments within guidance and control algorithms, with the aim of improving the efficiency, safety, and autonomy of these manoeuvres. The brief presents several applications of model predictive control to rendezvous manoeuvres, including Ankersen zero-order-hold particular solution1, which provides a realistic thrust profile. It offers new approaches for rendezvous manoeuvres in elliptical orbits, formulating obstacle avoidance constraints, passive safety constraints, and robustness techniques. It also compares finite-horizon and variable-horizon formulations for model predictive control in the context of performance and computational complexity. Predictive Control for Spacecraft Rendezvous is accessible to academics and students new to the topics of orbital rendezvous and model predictive control, but also presents compelling subject matter for researchers and professionals in the aerospace industry.

Author : Gerald R. Hintz
Publisher : Springer Nature
Page : 461 pages
File Size : 40,8 Mb
Release : 2023-01-11
Category : Technology & Engineering
ISBN : 9783030965730

Get Book

Orbital Mechanics and Astrodynamics by Gerald R. Hintz Pdf

Now in an updated second edition, this classroom-tested textbook covers fundamental and advanced topics in orbital mechanics and astrodynamics designed to introduce readers to the basic dynamics of space flight. The book explains concepts and engineering tools a student or practicing engineer can apply to mission design and navigation of space missions. Through highlighting basic, analytic, and computer-based methods for designing interplanetary and orbital trajectories, the text provides excellent insight into astronautical techniques and tools. The second edition includes new material on the observational basics of orbit determination, information about precision calculations for data used inflight, such as Mars 2020 with the Ingenuity Helicopter, and improvements in mission design procedures, including the automated design of gravity-assist trajectories. Orbital Mechanics and Astrodynamics: Techniques and Tools for Space Missions is ideal for students in astronautical or aerospace engineering and related fields, as well as engineers and researchers in space industrial and governmental research and development facilities, as well as researchers in astronautics.

Author : Kyle Alfriend,Srinivas Rao Vadali,Pini Gurfil,Jonathan How,Louis Breger
Publisher : Elsevier
Page : 403 pages
File Size : 45,5 Mb
Release : 2009-11-16
Category : Technology & Engineering
ISBN : 9780080559650

Get Book

Spacecraft Formation Flying by Kyle Alfriend,Srinivas Rao Vadali,Pini Gurfil,Jonathan How,Louis Breger Pdf

Space agencies are now realizing that much of what has previously been achieved using hugely complex and costly single platform projects—large unmanned and manned satellites (including the present International Space Station)—can be replaced by a number of smaller satellites networked together. The key challenge of this approach, namely ensuring the proper formation flying of multiple craft, is the topic of this second volume in Elsevier’s Astrodynamics Series, Spacecraft Formation Flying: Dynamics, control and navigation. In this unique text, authors Alfriend et al. provide a coherent discussion of spacecraft relative motion, both in the unperturbed and perturbed settings, explain the main control approaches for regulating relative satellite dynamics, using both impulsive and continuous maneuvers, and present the main constituents required for relative navigation. The early chapters provide a foundation upon which later discussions are built, making this a complete, standalone offering. Intended for graduate students, professors and academic researchers in the fields of aerospace and mechanical engineering, mathematics, astronomy and astrophysics, Spacecraft Formation Flying is a technical yet accessible, forward-thinking guide to this critical area of astrodynamics. The first book dedicated to spacecraft formation flying, written by leading researchers and professors in the field Develops the theory from an astrodynamical viewpoint, emphasizing modeling, control and navigation of formation flying satellites on Earth orbits Examples used to illustrate the main developments, with a sample simulation of a formation flying mission included to illustrate high fidelity modeling, control and relative navigation