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Revolutionizing Spacecraft Rendezvous with L-TSG

A new system enhances spacecraft rendezvous efficiency and safety in space missions.

Taehyeun Kim, Robin Inho Kee, Ilya Kolmanovsky, Anouck Girard

― 6 min read


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Table of Contents

Spacecraft rendezvous is a fancy term for when two spacecraft meet up in space. This can happen for many reasons, such as bringing supplies to a space station or transferring crew members between vehicles. Imagine trying to park your car right next to another vehicle – but instead of being on solid ground, you’re floating in the vast emptiness of space!

The main goal is for one spacecraft (let’s call it the "Chief") to stay on its path, while the other spacecraft (the "Deputy") uses its engines to get close enough without bumping into it or going too far away. This task isn't quite as easy as it sounds, particularly when there are rules that both spacecraft need to follow.

The Challenges of Rendezvous

Rendezvous isn't a straightforward mission. There are various challenges to consider, like making sure the Deputy stays a safe distance from the Chief. Think of it like trying to dance closely with someone at a party without stepping on their toes. To make things even trickier, the Deputy must manage its speed and the powerful thrust of its engines so that it doesn’t zoom past the Chief or crash into it.

In the past, astronauts had to do these rendezvous missions manually. They needed skill, precision, and a touch of luck. However, with the advancement of technology, we can now use automated systems to help make rendezvous missions safer and more efficient.

Automated Control Approaches

Thanks to the wonders of automation, we have developed different control approaches that help manage the paths of the Chief and Deputy spacecraft during a rendezvous mission. One popular method uses what is called an "artificial potential function" to create safe paths for the spacecraft. But, just like trying to solve a rubik's cube that has a mind of its own, applying this method can be complicated, especially when there are multiple rules to follow.

Another approach is called Model Predictive Control (MPC). This method looks ahead at the paths of both spacecraft to make real-time decisions. However, it can be like trying to catch a jellyfish with your bare hands—it's not always straightforward due to the complex calculations involved.

Introducing the Time Shift Governor

Enter the Time Shift Governor (TSG), a tool designed to help make the rendezvous process smoother by applying rules to the Chief spacecraft’s path. TSG generates a virtual path that the Deputy spacecraft can follow, ensuring it remains on course while following the rules. Imagine the TSG as a traffic light that tells the Deputy when to go, slow down, or stop so it can meet the Chief safely.

In a nutshell, the TSG uses a simple one-dimensional optimization problem to solve the potential issues that could arise during the rendezvous. By adjusting the timing of the Deputy's trajectory relative to the Chief, it helps to avoid unwanted surprises, like an awkward collision.

Enhancing Control with Machine Learning

As if that wasn't enough, enter the world of machine learning! Think of it as a super-smart assistant that learns from past experiences. A deep learning technique, called Long Short-Term Memory (LSTM), is used to enhance TSG.

The LSTM analyzes data from past missions and predicts the best course of action for the Deputy. It helps to speed up computations and keeps everything running without hiccups. So, instead of starting from scratch every time, our spacecraft now have a reliable learning buddy helping them along the way.

The Learning-Based Time Shift Governor

Now we call our new and improved system the Learning-based Time Shift Governor (L-TSG). This L-TSG combines the traditional TSG with the predictive capabilities of the LSTM. By training this system with past simulations, it can make educated guesses about the best way for the Deputy to approach the Chief.

This clever combination not only saves time during the rendezvous missions but also improves safety. It’s like having a GPS in your car that knows the fastest route based on real-time traffic data.

How the L-TSG Works

So, how does this whole thing actually work? The L-TSG uses data from previous space missions and training simulations to learn how to calculate the ideal time shift for the Deputy. Using a “sliding window” method, it continuously adjusts its predictions based on the Deputy’s moving position.

To ensure everything is running smoothly, the L-TSG also checks for any potential problems along the way. If it finds something amiss, it can revert back to the trusty old TSG method, just in case. This backup plan means less chance of failure and more chances to succeed.

The Importance of Simulation

Of course, before we send our spacecraft on a rendezvous mission, we have to test everything out. That's where simulation comes in. Think of it as a practice run before the big day. We simulate various scenarios with different initial positions for the Deputy spacecraft. This allows us to see how well L-TSG holds up under different conditions.

In essence, these simulations are like playing a video game where you try out different strategies before settling on the one that works best. We can figure out what’s likely to go right, what could go wrong, and how our spacecraft can achieve its mission successfully.

Real-World Applications

The capabilities of L-TSG are not just limited to theoretical missions. They have been tested in real-life scenarios, both in Low Earth Orbit (LEO) and the Molniya orbit. The LEO is where the International Space Station (ISS) lives, while the Molniya orbit has some of the most challenging conditions due to its highly elliptical path.

Through simulated missions in these orbits, L-TSG has demonstrated its ability to handle various constraints, ensuring that the Deputy spacecraft not only gets close to the Chief but also does so safely. It has shown an impressive ability to adjust the time shifts without causing any trouble, proving its reliability.

Achieving Safety and Efficiency

Ultimately, the goal of this entire process is to ensure that spacecraft can rendezvous quickly and safely. Thanks to the use of modern technology, particularly LSTM, the L-TSG minimizes the chances of any unwanted surprises along the way. By streamlining the calculations required to determine the best trajectory, it enables smoother and safer rendezvous missions.

The innovative approach combines the best of control strategies with machine learning's predictive abilities. It’s like having your cake and eating it too. With L-TSG, the time it takes to compute the best trajectory has been significantly reduced, making every moment count during critical missions.

Conclusion

The landscape of spacecraft rendezvous is changing. With the introduction of advanced control methods and learning models, we can look forward to more efficient and safer missions in the future. Thanks to the combination of techniques, our spacecraft can dance through the stars without stepping on each other's toes.

In summary, L-TSG has shown that with a little bit of creativity and technology, even the most complex problems can be approached with clarity and precision. Now, the only thing left is to keep sending our spacecraft on adventures as they navigate the vast expanse of space, ready to rendezvous with their partners in the great beyond!

Original Source

Title: Constrained Control for Autonomous Spacecraft Rendezvous: Learning-Based Time Shift Governor

Abstract: This paper develops a Time Shift Governor (TSG)-based control scheme to enforce constraints during rendezvous and docking (RD) missions in the setting of the Two-Body problem. As an add-on scheme to the nominal closed-loop system, the TSG generates a time-shifted Chief spacecraft trajectory as a target reference for the Deputy spacecraft. This modification of the commanded reference trajectory ensures that constraints are enforced while the time shift is reduced to zero to effect the rendezvous. Our approach to TSG implementation integrates an LSTM neural network which approximates the time shift parameter as a function of a sequence of past Deputy and Chief spacecraft states. This LSTM neural network is trained offline from simulation data. We report simulation results for RD missions in the Low Earth Orbit (LEO) and on the Molniya orbit to demonstrate the effectiveness of the proposed control scheme. The proposed scheme reduces the time to compute the time shift parameter in most of the scenarios and successfully completes rendezvous missions.

Authors: Taehyeun Kim, Robin Inho Kee, Ilya Kolmanovsky, Anouck Girard

Last Update: 2024-12-07 00:00:00

Language: English

Source URL: https://arxiv.org/abs/2412.05748

Source PDF: https://arxiv.org/pdf/2412.05748

Licence: https://creativecommons.org/licenses/by/4.0/

Changes: This summary was created with assistance from AI and may have inaccuracies. For accurate information, please refer to the original source documents linked here.

Thank you to arxiv for use of its open access interoperability.

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