Description: The spacecraft dynamics code achieves the following requirements in turn.
(1) give a set of orbital elements OE, find out the initial position R and speed V.
(2) according to the number of orbital elements, the orbital Orbit1 is drawn by algebraic equation.
(3) draw Orbit2 from differential equations based on the initial location and speed.
(4) transform the Orbit1 of the plane into the Orbit3 of space and compare it with Orbit2.
(5) convert the Orbit2 of space to Orbit4 and compare it with Orbit1.
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File list (Check if you may need any files):
| Filename | Size | Date |
|---|
| Differential.m | 315 | 2017-10-27
|
| bh1.m | 8607 | 2017-10-31 |
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