The EDS was developed to provide a force of around 40mN at 40 cm coil-to-coil distance. It hardly adds up to 20% of the total weight of the module. The number of windings, coil radius and other current specifications depend on the type of mission or structure and can be calculated using the Sequential Least Squares Programming constrained to meet the minimization of weight and power consumption. The Active Docking module consists of a Seal Ring, to avoid leakage of breathable air after opening of hatch. It also consists of 12 pairs of electrically controlled autonomous latches to ensure a safe and perfect docking. The Latch Arm fixes itself into the Latch Capture Space on the Passive Docking Module, and compresses the seal ring, made of silicone preferably, to provide a proper seal. Alignment procedures are carried out autonomously by the on-board Attitude Determination and Control System.
For undocking, currents are flown in opposite directions in both the coils to allow repulsion, after unlocking the latches autonomously.
The electromagnetic attraction and repulsion allow a propellant free docking and undocking procedure. Electromagnetism provides a wider capture range for the Passive Docking Module, that clearly gives it a upper hand over the current docking mechanisms. It is cost-friendly since its propellant free and uses lesser components than the current docking mechanisms. However, it has a higher power consumption than other mechanisms, which can be tackled by inventing more efficient batteries that can boost the production of electricity through solar energy and meet the needs of this mechanism.
Electromagnetic Docking can significantly influence in-space assembly of larger telescopes.
Aethereal Tech hopes to achieve or at least help to realize this advancement in space tech that can help us achieve our dream of becoming a multiplanetary species.
Our team, Aethereal Tech, consists of designers and technophiles. When I stumbled across this idea Let's Connect, I suggested it to my team and they approved of it, since we lacked coders and thus weren't eligible for solving coding problems, though it wasn't the reason why we chose this. We share a common admiration towards space tech and that was the driving force for us to sit down and create. After reading several research papers on Electromagnetic Docking, we realized that the idea is well established for smaller missions.
In order to implement this to bigger structures, we carefully studied the fundamentals surrounding this technology over the course of a few weeks, before the hackathon. We learned a great deal about the various onboard systems like Continuous Differential GPS and the different instruments involved in the Attitude Determination and Control System and their uses in everyday space operations.
We barely started with our Fresher classes before the hackathon. Equipped only with high school science, we decided to make the best of the situation and started interpreting online resources. This is how we materialized our project. It is justified to say that we learned a lot throughout these few weeks, and we had a great time collaborating with each other, constructing upon the ideas of 6 creative brains.
We used the agencies' website and other resources to understand their docking mechanisms. It is crucial to understand the existing technologies in order to formulate the improvements that can be implemented. We browsed through the resources provided to us on the NASA Space Apps Challenge website and learned about in-space assembly. EDS helps in the in-space assembly of smaller components of, say a higher aperture space telescope. Overall, the websites of NASA and ESA helped to gain additional knowledge about their docking mechanisms and their visions for the future of docking and rendezvous technology.
authors.library.caltech.edu
www.jstage.jst.go.jp
Attitude Determination and Control System (ADCS)
www.tudelft.nl
Small Satellite Electromagnetic Docking System Modeling and Control | ASU Digital Repository
repository.asu.edu
www.nasa.gov
A new docking system for space rendezvous | maxon group
www.maxongroup.in