question-mark
Stuck on an issue?

Lightrun Answers was designed to reduce the constant googling that comes with debugging 3rd party libraries. It collects links to all the places you might be looking at while hunting down a tough bug.

And, if you’re still stuck at the end, we’re happy to hop on a call to see how we can help out.

Relative motion, phasing, rendez-vous

See original GitHub issue

🎯 Goal

💡 Possible solutions

📋 Steps to solve the problem

  • Comment below about what you’ve started working on.
  • Add, commit, push your changes
  • Submit a pull request and add this in comments - Addresses #<put issue number here>
  • Ask for a review in comments section of pull request
  • Celebrate your contribution to this project 🎉

Issue Analytics

  • State:open
  • Created 6 years ago
  • Comments:6 (6 by maintainers)

github_iconTop GitHub Comments

3reactions
astrojuanlucommented, May 1, 2021

I am back three years late on this topic, so I must apologise, and hope it is not to late to make a contribution in this area 😃

Sometimes the pace of open source is slow 😃 But I’m so happy that you still want to contribute!

I have created a rough sample of a basic relative orbit object class, do you think this structure is OK?

Now that we have our contrib/ directory, what do you think about adding there relative_eccentricity_vector(...) and relative_inclination_vector first, before we go any further? This way we can also identify which parts could be moved to poliastro.core at the same time we review it. I am not so sure what sampling would do, but I’m sure I will understand it better when I see the other two 😃 And also, the plot function will probably be useful! But again, let’s go step by step so the review is palatable 😄

0reactions
sammmlowcommented, May 31, 2021

I’m thinking if we might like to see a core relative_orbit class, that can be called as a separate module under poliastro.twobody? What do you think Juan? I could do up the docs for it too 😃

Read more comments on GitHub >

github_iconTop Results From Across the Web

Relative Motion: Terminal Phase Rendezvous | N-body Physics
The relative motion framework determines the maneuver required to get to any position with respect to the target. In rendezvous scenarios a cautious...
Read more >
Rendezvous Maneuver - an overview | ScienceDirect Topics
This chapter illustrates an elative motion analysis to gain familiarity with the problem of maneuvering one spacecraft relative to another, especially when they ......
Read more >
Relative Motion in the Docking Phase of Orbital Rendezvous
The purpose of this report is to analyze the relative motion which exists between an interceptor and target vehicle in the final stages...
Read more >
Discrete-Variable-Thrust Guidance for Orbital Rendezvous ...
Relative Orbital Motion. Orbital rendezvous involves an actively controlled spacecraft, i.e. the chaser, and a passive spacecraft, ...
Read more >
Trajectory control with continuous thrust applied ... - IOPscience
This paper will focus on close range rendezvous phase, which can be divided into two sub- ... analyze the relative motion for several...
Read more >

github_iconTop Related Medium Post

No results found

github_iconTop Related StackOverflow Question

No results found

github_iconTroubleshoot Live Code

Lightrun enables developers to add logs, metrics and snapshots to live code - no restarts or redeploys required.
Start Free

github_iconTop Related Reddit Thread

No results found

github_iconTop Related Hackernoon Post

No results found

github_iconTop Related Tweet

No results found

github_iconTop Related Dev.to Post

No results found

github_iconTop Related Hashnode Post

No results found