Decelerating a Constantly Accelerating Ship

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SUMMARY

The discussion centers on calculating the optimal point to decelerate a spacecraft traveling 20 light years away while simulating varying acceleration rates of 1g to 3g. The contributor determined that with a constant 1g acceleration, deceleration should begin at approximately 10 light years, with a total travel time of about 3.023 years as measured on the spacecraft. For varying acceleration, numerical integration is necessary to accurately model the changing rates. The equations for constant acceleration can be found at the provided link.

PREREQUISITES
  • Understanding of special relativity and its implications on time and distance.
  • Familiarity with calculus, specifically integration techniques.
  • Knowledge of spacecraft dynamics and acceleration principles.
  • Experience with numerical methods for solving differential equations.
NEXT STEPS
  • Study the equations of motion under constant acceleration from the provided resource.
  • Learn numerical integration techniques applicable to varying acceleration scenarios.
  • Explore advanced topics in special relativity related to time dilation and length contraction.
  • Investigate spacecraft propulsion systems capable of sustained acceleration.
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Aerospace engineers, physicists, and enthusiasts interested in spacecraft navigation and relativistic travel dynamics will benefit from this discussion.

zeframcochrane
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This is simply a thought experiment.

Say that I had a spacecraft capable of constantly accelerating or decelerating at a rate of 1g to 3g. I want to hit a target 20 light years away. How would I know where along the way to turn the ship around if I wanted to end at my destination decelerating at a rate of 3g. I have worked out that with a constant rate of acceleration (for example 1g) I would have to begin decelerating at 10 Lr. The catch here is that I want to change the rate of acceleration or deceleration gradually along the trip to eventually simulate 3g aboard the ship.

I've been building a dynamically modeled system to answer my question but there must be an easier way. I think I have to integrate my rate of acceleration over a set of points, but its been awhile since I took calculus. Any takers?
 
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The equations you need for any constant acceleration are given at:

http://www.desy.de/user/projects/Physics/Relativity/SR/rocket.html

For a case similar to yours where you assume constant 1g acceleration, followed by constant 1g deceleration, such that you end at rest 20 ly away in your starting frame, then you would reverse thrust after 3.023... years as measured on your rocket's clocks. Saying 10 light years as in your initial frame isn't useful because how would you identify this point in the rocket (unless there were a marker there)?

For varying acceleration, there is no avoiding calculus, and you may need numerical integration.
 

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