Automated Rendezvous and Docking of Spacecraft
This definitive reference for space engineers provides an overview of the major issues governing approach and mating strategies, and system concepts for rendezvous & docking/berthing (RVD/B).
TABLE OF CONTENTS Automated Rendezvous and Docking of Spacecraft
Chapter 8: Mating Systems
The objective of this chapter is to provide a basic understanding of the dynamic and kinematic processes which are taking place during docking or berthing of two vehicles, and to give an overview of the design principles used for docking and berthing mechanisms. Design driving requirements for these mechanisms are briefly discussed, and an overview of existing mechanism developments is given. The dynamic processes of contact and capture at docking are discussed using a simple model of an equivalent mass, which represents the masses of both spacecraft plus a central attenuation system. Basic functional concepts of the design elements used for shock attenuation, capture, structural connection and sealing are discussed at the end of the chapter.
8.1 Basic concepts of docking and berthing
The main tasks and issues arising during docking and berthing have already been addressed in section 2.5. Definitions of the terms 'docking' and 'berthing' have been given in chapter 1. For completeness of this chapter, these key definitions shall be recalled here.
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As a general term for the process of achieving contact, capture and connection, the term mating is used. This includes the two cases 'docking' and 'berthing'.
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The term docking is used for the case where the GNC system of the chaser controls the required vehicle state parameters necessary to ensure that its capture interfaces enter into those of the target vehicle, and where the capture location is also the location for structural connection.
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The term berthing is used for the case, where
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