Undergrad Calculate Voyager trajectory using JPL data

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SUMMARY

This discussion focuses on calculating the trajectories of Voyager 1 and Voyager 2 using data from the JPL database. The user has successfully simulated the solar system's core elements and seeks to incorporate the Voyagers' trajectories by analyzing gravitational effects and thrusts. The proposed method involves comparing calculated trajectories with JPL data, specifically using the Horizons system to obtain position and velocity data for specific dates, such as June 1 and July 1. The approach emphasizes integrating spacecraft positions to identify any thrust events based on velocity differences.

PREREQUISITES
  • Understanding of gravitational calculations and perturbations
  • Familiarity with JPL Horizons system for spacecraft data
  • Knowledge of trajectory simulation techniques
  • Basic programming skills for implementing simulations
NEXT STEPS
  • Learn how to use JPL Horizons to retrieve spacecraft position and velocity data
  • Study gravitational perturbation calculations for celestial bodies
  • Explore numerical integration methods for trajectory analysis
  • Investigate thrust modeling techniques used in spacecraft missions
USEFUL FOR

Aerospace engineers, astrophysicists, and developers working on space simulation projects will benefit from this discussion, particularly those interested in trajectory calculations and spacecraft dynamics.

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Hey everyone,

I've recently programmed an animated simulation of the main elements (core planets and Sun) of our solar system: by using the initial coordinates from the JPL database, and then calculating the combined gravitational perturbations and the relativistic effects from the Sun.

However I would now like to calculate the trajectories for both Voyager 1 & 2, and then map them onto my simulation. I can easily replicate the gravitational calculations used for the planets and the Sun, but I'm afraid I'm struggling to find, or figure out how to replicate the various thrusts used throughout the voyagers' mission.

Current thought: Calculate voyagers trajectory purely using gravitational effects and initial position/velocity, and then compare calculated data with JPL data, taking into account error, to calculate any unnatural changes in velocity (i.e. thrusts).

Any thoughts, insights or advice would be much appreciated, thank-you.
 
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Get Horizons position and velocity for any 2 dates and place in simulation. Let's use June 1 and July 1 for example.
Import June 1 data. Integrate to July 1, and import July 1 data. You now have 2 spacecraft in your sim. Are the spacecraft in the same place traveling at the same speed? If so, then no thrust was applied during this time period. If they differ, integrate backwards until they make their closest approach to each other. That will give you the date of the burn. The difference in velocity at this point will tell you the delta v.
 
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