image thumbnail


version (2.06 KB) by Brandon
Determine Arrival Velocity of a Orbiting Object


Updated 19 May 2014

View License

This function determines the arrival velocity of an orbit for a given initial position and velocity and arrival position
r1 - initial position
v1 - initial velocity
r2 - arrival position
mu - gravitational parameter
v2 - arrival velocity
The units of the input variables must agree. Examples include: (km & s),
(DU & TU), etc

Cite As

Brandon (2022). DetermineVArrival.m (, MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2013b
Compatible with any release
Platform Compatibility
Windows macOS Linux

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!