AE 4532 - Spacecraft Flight Dynamics Functions
These are MATLAB functions I made while taking AE 4532 (Spacecraft flight dynamics) at Georgia Tech.
So far, the following subjects are covered:
- 2 body problem
- Numerical solver
- Solution of Kepler's equation
- Ideal interplanetary transfers
- Rotation matrices
- Creation from euler angles
- Conversion to/from axis-angle representation and quaternions
- Conversion to zxz, xyz euler angles
- Response to constant torque
- Of angular velocity (also for time-dependent torque)
- Of rotation matrices
- Of xyz, zxz euler angles
- Misc
- Databse of constants and orbital parameters for major solar system bodies