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This function determines the arrival velocity of an orbit for a given initial position and velocity and arrival position
Inputs:
r1 - initial position
v1 - initial velocity
r2 - arrival position
mu - gravitational parameter
Outputs:
v2 - arrival velocity
The units of the input variables must agree. Examples include: (km & s),
(DU & TU), etc
Cite As
Brandon (2026). DetermineVArrival.m (https://www.mathworks.com/matlabcentral/fileexchange/46650-determinevarrival-m), MATLAB Central File Exchange. Retrieved .
General Information
- Version 1.0.0.0 (2.06 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 1.0.0.0 |
