Orbital simulator and non fixed orbit

In summary, the conversation discusses a 3 planet system, with one planet being fixed and significantly heavier than the others. The simulation of the system shows that one of the moving planets has a variable orbit, while the other has a fixed elliptic orbit. The other planet in the system also has a fixed elliptic orbit, and its distance and weight are described. The variation in one of the planet's orbit is attributed to potential interactions with the other planets.
  • #1
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Hello,
Let's consider a small 3 planet system. One of the planet's is fixed and is a lot heavier than the others. The acelleration is
mP2 * aP2 = - FP3 - FP1
From with the velocity is derived with allows to calculate the positions of the planet's in a simulator program. After running the simulation, The orbit of one of the "moving" planets isn't fixed - some variation occur after each loop.

What can cause this? The other planet (that's not fixed) has an elliptic fixed orbit.
FP = Gravitational Force of Planet
Thanks.
 
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  • #2
Hello,
some more data about the situation:

Planet 1 - fixed on the center of the referential
Planet 2 - initial distance = 3 AU (start_x= 3 AU, start_y = 0)
Planet 3 - initial distance = 6 AU (start_x= 6 AU, start_y=0)

So Planet 2 is on the "middle" of the system.

Planet 1 is about 1000 times "heavier" than Planet 2.
Planet 3 is about 30 times "heavier" than Planet 2.

Planet 3's orbit is fixed elliptic. Planet 2's orbit has some variation to the initial elliptic orbit.

1) I was under the impression that orbits were suposed to be fixed...
2) I'm guessing the planet in the "middle" is getting heavy interaction from the other planet's...

Thanks for your comments.
 
  • #3


There are a few possible causes for the non-fixed orbit in your simulation. One possibility is that there are external forces acting on the planet, such as gravitational forces from other bodies in the system or non-uniform density distributions within the planet itself. Another possibility is that there are numerical errors or approximations in the simulation program, which can lead to small variations in the orbital path over time. It is also important to consider the initial conditions and parameters used in the simulation, as these can greatly affect the stability of the orbits. Further analysis and adjustments to these factors may help to improve the accuracy and fixedness of the orbits in your simulation.
 

1. What is an orbital simulator?

An orbital simulator is a computer program or software that allows users to simulate and visualize the motion and behavior of objects in orbit around a central body, such as a planet or star. It takes into account various factors such as gravity, velocity, and trajectory to accurately depict the orbit of an object.

2. How does an orbital simulator work?

An orbital simulator uses mathematical equations and algorithms to calculate the motion of objects in orbit. It takes into account the laws of physics, such as Newton's laws of motion and the law of universal gravitation, to determine the trajectory and velocity of objects in orbit. This information is then translated into a visual representation for the user to view.

3. What is a non-fixed orbit?

A non-fixed orbit refers to an orbit that is not perfectly circular or elliptical, but instead has variations or irregularities in its shape. This could be caused by factors such as gravitational pull from other objects, atmospheric drag, or external forces acting on the orbiting object.

4. Can an orbital simulator be used for any object in orbit?

Yes, an orbital simulator can be used for any object in orbit around a central body. This includes natural objects such as planets, moons, and asteroids, as well as artificial satellites and spacecraft. The accuracy of the simulation may vary depending on the available data and the complexity of the orbit.

5. What are the practical applications of an orbital simulator?

An orbital simulator has many practical applications, such as predicting and planning satellite orbits for communication and navigation purposes, simulating space missions for research and exploration, and studying the behavior of objects in the solar system. It can also be used to train astronauts and spacecraft operators, as well as for educational purposes.

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