DVLowThrust:

Path: Orbit/OrbitManeuver

% Delta-V from a circular to noncoplanar circular orbit.
 Compute the velocity change for a transfer from a circular orbit
 to a noncoplanar circular orbit. vI or vF or dI may be a vector.

 Type  DVLowThrust for a demo from LEO to GEO.

------------------------------------------------------------------------
   Form:
   dV = DVLowThrust( vI, vF, dI )
------------------------------------------------------------------------

   ------
   Inputs
   ------
   vI      (1,:)     Initial velocity
   vF      (1,:)     Final velocity
   dI      (1,:)     Change in inclination (rad)

   -------
   Outputs
   -------
   dV      (1,:)     Velocity change

------------------------------------------------------------------------

Children:

Common: Graphics/Plot2D

---

Back to the Orbit Module page