Paper
19 May 2005 Autonomous docking system for space structures and satellites
Guru Prasad, Eddie Tajudeen, James Spenser
Author Affiliations +
Abstract
Aximetric proposes Distributed Command and Control (C2) architecture for autonomous on-orbit assembly in space with our unique vision and sensor driven docking mechanism. Aximetric is currently working on ip based distributed control strategies, docking/mating plate, alignment and latching mechanism, umbilical structure/cord designs, and hardware/software in a closed loop architecture for smart autonomous demonstration utilizing proven developments in sensor and docking technology. These technologies can be effectively applied to many transferring/conveying and on-orbit servicing applications to include the capturing and coupling of space bound vehicles and components. The autonomous system will be a “smart” system that will incorporate a vision system used for identifying, tracking, locating and mating the transferring device to the receiving device. A robustly designed coupler for the transfer of the fuel will be integrated. Advanced sealing technology will be utilized for isolation and purging of resulting cavities from the mating process and/or from the incorporation of other electrical and data acquisition devices used as part of the overall smart system.
© (2005) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Guru Prasad, Eddie Tajudeen, and James Spenser "Autonomous docking system for space structures and satellites", Proc. SPIE 5799, Modeling, Simulation, and Verification of Space-based Systems II, (19 May 2005); https://doi.org/10.1117/12.606169
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CITATIONS
Cited by 3 scholarly publications.
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KEYWORDS
Sensors

Control systems

Space operations

Computer aided design

Satellites

Connectors

Computer simulations

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