Guidance Navigation And Control For Spacecraft Rendezvous And Docking Theory And Methods

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Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods

Yongchun Xie,Changqing Chen,Tao Liu,Min Wang
Guidance Navigation and Control for Spacecraft Rendezvous and Docking Theory and Methods Book PDF

Author : Yongchun Xie,Changqing Chen,Tao Liu,Min Wang
Publisher : Springer Nature
Page : 495 pages
File Size : 44,6 Mb
Release : 2021-02-16
Category : Technology & Engineering
ISBN : 9789811569906

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Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods by Yongchun Xie,Changqing Chen,Tao Liu,Min Wang Pdf

This book focuses on the theory and design methods for guidance, navigation, and control (GNC) in the context of spacecraft rendezvous and docking (RVD). The position and attitude dynamics and kinematics equations for RVD are presented systematically in accordance with several different coordinate systems, including elliptical orbital frame, and recommendations are supplied on which of these equations to use in different phases of RVD. The book subsequently explains the basic principles and relative navigation algorithms of RVD sensors such as GNSS, radar, and camera-type RVD sensors. It also provides guidance algorithms and schemes for different phases of RVD, including the latest research advances in rapid RVD. In turn, the book presents a detailed introduction to intelligent adaptive control and proposes corresponding theoretical approaches to thruster configuration and control allocation for RVD. Emphasis is placed on the design method of active and passive trajectory protection in different phases of RVD, and on the safety design of the RVD mission as a whole. For purposes of verification, the Shenzhou spacecraft’s in-orbit flight mission is introduced as well. All issues addressed are described and explained from basic principles to detailed engineering methods and examples, providing aerospace engineers and students both a basic understanding of, and numerous practical engineering methods for, GNC system design in RVD.

Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods

Yongchun Xie,Changqing Chen,Tao Liu,Min Wang
Guidance Navigation and Control for Spacecraft Rendezvous and Docking Theory and Methods Book PDF

Author : Yongchun Xie,Changqing Chen,Tao Liu,Min Wang
Publisher : Unknown
Page : 0 pages
File Size : 41,9 Mb
Release : 2021
Category : Electronic
ISBN : 9811569916

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Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods by Yongchun Xie,Changqing Chen,Tao Liu,Min Wang Pdf

This book focuses on the theory of and design methods for guidance, navigation, and control (GNC) in the context of spacecraft rendezvous and docking (RVD). The position and attitude dynamics and kinematics equations for RVD are presented systematically and in accordance with several different coordinate systems, including elliptical orbital frame, and recommendations are supplied on which of these equations to use in different phases of RVD. The book subsequently explains the basic principles and relative navigation algorithms of RVD sensors such as GNSS, radar, and camera-type RVD sensors. It also provides guidance algorithms and schemes for different phases of RVD, including the latest research advances in rapid RVD. In turn, the book presents a detailed introduction to intelligent adaptive control and proposes corresponding theoretical approaches to thruster configuration and control allocation for RVD. Emphasis is placed on the design method of active and passive trajectory protection in different phases of RVD, and on the safety design of the RVD mission as a whole. For purposes of verification, the Shenzhou spacecraft's in-orbit flight mission is presented as well. All issues addressed are described and explained from basic principles to detailed engineering methods and examples, providing aerospace engineers and students both a basic understanding of, and numerous practical engineering methods for, GNC system design in RVD. .

Guidance and Control of a Spacecraft to Rendevous and Dock with a Non-cooperative Target

Anantha Sayanam Komanduri
Guidance and Control of a Spacecraft to Rendevous and Dock with a Non cooperative Target Book PDF

Author : Anantha Sayanam Komanduri
Publisher : Cuvillier Verlag
Page : 210 pages
File Size : 40,7 Mb
Release : 2011-11-22
Category : Technology & Engineering
ISBN : 9783736939455

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Guidance and Control of a Spacecraft to Rendevous and Dock with a Non-cooperative Target by Anantha Sayanam Komanduri Pdf

Non-cooperative spacecrafts are those current or future assets in orbit which have lost their control authority in one or more degrees of freedom and cannot convey any information concerning their position, attitude or rates to facilitate Rendezvous and Docking/Berthing (RVD/B) process. A growing field of study in space research is to develop On-Orbit Servicing (OOS) technology capable of dealing with these space- crafts, called targets, which are designed without any intention to be serviced. To render services such as repair, refuel or removal of the target from orbit, the chaser spacecraft should exhibit sophisticated RVD/B technology for formation fly and final stage docking/berthing operations of the mission. Assuming that the terminal capture operations of the target are to be performed by a suitable manipulator system on-board chaser, this study relies upon proven technology and outlines guidance and control methodologies to achieve rendezvous during proximity phases. The entry gate of chaser after phasing can be defined at a distance of about 5 km in ± V-bar direction from the target in its orbit. To account for errors in modeling, navigation or actuation, proximity range operations from the entry gate are decomposed into three different subphases as far range, inspection or fly around and closer approach. From the entry gate and along the path of the chaser two hold points are defined: first to initiate an inspection and the second, which is close to the safe zone defined around the target, to initiate a capture. The chaser is assumed to perform a station keeping maneuver at the second hold point until initial conditions for the capture are met. Possible scenarios pertaining to the behavior of the target in a circular orbit are considered and guidance schemes for different subphases are presented using a combination of Hill-Clohessy-Willtshire (HCW) solution, elliptical fly around, glides- lope algorithm etc. Relative controllers both for position and attitude of the chaser are also presented. A Linear Quadratic (LQ) controller for relative position and a Proportional Integral Derivative (PID) controller for relative attitude with angular velocity constraints are chosen to track down the error to achieve rendezvous and attitude synchronization with the non-cooperative target. A comparative analysis between different guidance trajectories for important parameters such as time, fuel usage, minimum absolute distance and the maximum radial distance from the target is presented. Verification of the proposed guidance and control methods is done by applying them to two different case studies: the first study incorporating a stabilized target in Geostationary Earth Orbit (GEO) and the second, with a spinning target in Low Earth Orbit (LEO). The methods presented here are general and provide a simulator to the chaser to perform rendezvous analysis with non-cooperative targets. To achieve RVD/B, the study proposes a careful combination of guidance solutions for different phases of proximity operations, and for different scenario’s of the target encountered by the chaser.

Proceedings of the 44th Annual American Astronautical Society Guidance, Navigation, and Control Conference, 2022

Matt Sandnas
Proceedings of the 44th Annual American Astronautical Society Guidance Navigation and Control Conference 2022 Book PDF

Author : Matt Sandnas
Publisher : Springer Nature
Page : 1809 pages
File Size : 41,6 Mb
Release : 2024
Category : Flight control
ISBN : 9783031519284

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Proceedings of the 44th Annual American Astronautical Society Guidance, Navigation, and Control Conference, 2022 by Matt Sandnas Pdf

Zusammenfassung: This conference attracts GN&C specialists from across the globe. The 2022 Conference was the 44th Annual GN&C conference with more than 230 attendees from six different countries with 44 companies and 28 universities represented. The conference presented more than 100 presentations and 16 posters across 18 topics. This year, the planning committee wanted to continue a focus on networking and collaboration hoping to inspire innovation through the intersection of diverse ideas. These proceedings present the relevant topics of the day while keeping our more popular and well-attended sessions as cornerstones from year to year. Several new topics including "Autonomous Control of Multiple Vehicles" and "Results and Experiences from OSIRIS-REx" were directly influenced by advancements in our industry. In the end, the 44th Annual GN&C conference became a timely reflection of the current state of the GN&C ins the space industry. The annual American Astronautical Society Rocky Mountain Guidance, Navigation and Control (GN&C) Conference began 1977 as an informal exchange of ideas and reports of achievements among guidance and control specialists local to the Colorado area. Bud Gates, Don Parsons, and Bob Culp organized the first conference, and began the annual series of meetings the following winter. In March 1978, the First Annual Rocky Mountain Guidance and Control Conference met at Keystone, Colorado. It met there for eighteen years, moving to Breckenridge in 1996 where it has been for over 25 years

Predictive Control for Spacecraft Rendezvous

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

Author : Afonso Botelho,Baltazar Parreira,Paulo N. Rosa,João Miranda Lemos
Publisher : Springer Nature
Page : 116 pages
File Size : 53,5 Mb
Release : 2021-06-24
Category : Technology & Engineering
ISBN : 9783030756963

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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.

Control, Guidance and Navigation of Spacecraft

NASA-University Conference on the Science and Technology of Space Exploration, Chicago, 1962
Control Guidance and Navigation of Spacecraft Book PDF

Author : NASA-University Conference on the Science and Technology of Space Exploration, Chicago, 1962
Publisher : Unknown
Page : 64 pages
File Size : 51,7 Mb
Release : 1963
Category : Navigation (Astronautics)
ISBN : UVA:X002570624

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Control, Guidance and Navigation of Spacecraft by NASA-University Conference on the Science and Technology of Space Exploration, Chicago, 1962 Pdf

Control, Guidance, and Navigation of Spacecraft

United States. National Aeronautics and Space Administration
Control Guidance and Navigation of Spacecraft Book PDF

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 64 pages
File Size : 53,5 Mb
Release : 1962
Category : Navigation (Astronautics)
ISBN : STANFORD:36105024705217

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Control, Guidance, and Navigation of Spacecraft by United States. National Aeronautics and Space Administration Pdf

Automated Rendezvous and Docking of Spacecraft

Wigbert Fehse
Automated Rendezvous and Docking of Spacecraft Book PDF

Author : Wigbert Fehse
Publisher : Cambridge University Press
Page : 517 pages
File Size : 42,5 Mb
Release : 2003-11-13
Category : Technology & Engineering
ISBN : 9781139440684

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Automated Rendezvous and Docking of Spacecraft by Wigbert Fehse Pdf

The definitive reference for space engineers on rendezvous and docking/berthing (RVD/B) related issues, this book answers key questions such as: How does the docking vehicle accurately approach the target spacecraft? What technology is needed aboard the spacecraft to perform automatic rendezvous and docking, and what systems are required by ground control to supervise this process? How can the proper functioning of all rendezvous-related equipment, systems and operations be verified before launch? The book provides an overview of the major issues governing approach and mating strategies, and system concepts for rendezvous and docking/berthing. These issues are described and explained such that aerospace engineers, students and even newcomers to the field can acquire a basic understanding of RVD/B. The author would like to extend his thanks to Dr Shufan Wu, GNC specialist and translator of the book's Chinese edition, for his help in the compilation of these important errata.

Advances in Guidance, Navigation and Control

Liang Yan,Haibin Duan,Xiang Yu
Advances in Guidance Navigation and Control Book PDF

Author : Liang Yan,Haibin Duan,Xiang Yu
Publisher : Springer Nature
Page : 5416 pages
File Size : 49,5 Mb
Release : 2021-11-12
Category : Technology & Engineering
ISBN : 9789811581557

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Advances in Guidance, Navigation and Control by Liang Yan,Haibin Duan,Xiang Yu Pdf

This book features the latest theoretical results and techniques in the field of guidance, navigation, and control (GNC) of vehicles and aircraft. It covers a range of topics, including, but not limited to, intelligent computing communication and control; new methods of navigation, estimation, and tracking; control of multiple moving objects; manned and autonomous unmanned systems; guidance, navigation, and control of miniature aircraft; and sensor systems for guidance, navigation, and control. Presenting recent advances in the form of illustrations, tables, and text, it also provides detailed information of a number of the studies, to offer readers insights for their own research. In addition, the book addresses fundamental concepts and studies in the development of GNC, making it a valuable resource for both beginners and researchers wanting to further their understanding of guidance, navigation, and control.

Research and Technology Program Digest

United States. National Aeronautics and Space Administration
Research and Technology Program Digest Book PDF

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 792 pages
File Size : 46,9 Mb
Release : 2024-06-03
Category : Electronic
ISBN : STANFORD:36105112109157

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Research and Technology Program Digest by United States. National Aeronautics and Space Administration Pdf

Spacecraft Modeling, Attitude Determination, and Control

Yaguang Yang
Spacecraft Modeling Attitude Determination and Control Book PDF

Author : Yaguang Yang
Publisher : CRC Press
Page : 328 pages
File Size : 42,7 Mb
Release : 2019-02-06
Category : Science
ISBN : 9780429822148

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Spacecraft Modeling, Attitude Determination, and Control by Yaguang Yang Pdf

This book discusses all spacecraft attitude control-related topics: spacecraft (including attitude measurements, actuator, and disturbance torques), modeling, spacecraft attitude determination and estimation, and spacecraft attitude controls. Unlike other books addressing these topics, this book focuses on quaternion-based methods because of its many merits. The book lays a brief, but necessary background on rotation sequence representations and frequently used reference frames that form the foundation of spacecraft attitude description. It then discusses the fundamentals of attitude determination using vector measurements, various efficient (including very recently developed) attitude determination algorithms, and the instruments and methods of popular vector measurements. With available attitude measurements, attitude control designs for inertial point and nadir pointing are presented in terms of required torques which are independent of actuators in use. Given the required control torques, some actuators are not able to generate the accurate control torques, therefore, spacecraft attitude control design methods with achievable torques for these actuators (for example, magnetic torque bars and control moment gyros) are provided. Some rigorous controllability results are provided. The book also includes attitude control in some special maneuvers, such as orbital-raising, docking and rendezvous, that are normally not discussed in similar books. Almost all design methods are based on state-spaced modern control approaches, such as linear quadratic optimal control, robust pole assignment control, model predictive control, and gain scheduling control. Applications of these methods to spacecraft attitude control problems are provided. Appendices are provided for readers who are not familiar with these topics.

Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems

Runqi Chai,Al Savvaris,Antonios Tsourdos,Senchun Chai
Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems Book PDF

Author : Runqi Chai,Al Savvaris,Antonios Tsourdos,Senchun Chai
Publisher : Springer
Page : 207 pages
File Size : 47,6 Mb
Release : 2019-07-30
Category : Technology & Engineering
ISBN : 9789811398452

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Design of Trajectory Optimization Approach for Space Maneuver Vehicle Skip Entry Problems by Runqi Chai,Al Savvaris,Antonios Tsourdos,Senchun Chai Pdf

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.