File:FlightPathAngle.svg
Summary
| Description |
English: The position and velocity of a satellite in orbit about a central body. The velocity is depicted with its transversal and radial component, the flight path angle phi and true anomaly nu are mentioned. p is the semiparameter, a the semimajor axis and b the semiminor axis of the ellipse. This illustrates the Kepler laws and the solution of the Two-body problem. |
| Date | |
| Source | Own work |
| Author | Åntøinæ |
Licensing
I, the copyright holder of this work, hereby publish it under the following license:
This file is licensed under the Creative Commons Attribution-Share Alike 4.0 International license.
- You are free:
- to share – to copy, distribute and transmit the work
- to remix – to adapt the work
- Under the following conditions:
- attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
- share alike – If you remix, transform, or build upon the material, you must distribute your contributions under the same or compatible license as the original.
